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PG 9 JI Proc. IEEE PY 1989 PD NOV VL 77 IS 11 GA CL319 J9 PROC IEEE UT ISI:A1989CL31900004 PT J AU EVANS, J TURNBULL, D TI DEVELOPMENT OF AN AUTOMATED WINDSHEAR DETECTION SYSTEM USING DOPPLER WEATHER RADAR SO PROCEEDINGS OF THE IEEE BP 1661 EP 1673 PG 13 JI Proc. IEEE PY 1989 PD NOV VL 77 IS 11 GA CL319 J9 PROC IEEE UT ISI:A1989CL31900008 PT J AU MASSOGLIA, PL POZESKY, MT GERMANA, GT TI THE USE OF SATELLITE TECHNOLOGY FOR OCEANIC AIR-TRAFFIC-CONTROL SO PROCEEDINGS OF THE IEEE BP 1695 EP 1708 PG 14 JI Proc. IEEE PY 1989 PD NOV VL 77 IS 11 B-48 GA CL319 J9 PROC IEEE UT ISI:A1989CL31900011 PT J AU WILLIAMSON, T SPENCER, NA TI DEVELOPMENT AND OPERATION OF THE TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) SO PROCEEDINGS OF THE IEEE BP 1735 EP 1744 PG 10 JI Proc. IEEE PY 1989 PD NOV VL 77 IS 11 GA CL319 J9 PROC IEEE UT ISI:A1989CL31900014 PT J AU FABRY, JM LUPINETTI, AA TI APPLICATIONS OF SIMULATION AND ARTIFICIAL-INTELLIGENCE TECHNOLOGY FOR ATC TRAINING SO PROCEEDINGS OF THE IEEE BP 1762 EP 1765 PG 4 JI Proc. IEEE PY 1989 PD NOV VL 77 IS 11 GA CL319 J9 PROC IEEE UT ISI:A1989CL31900017 PT J
AU MASON, RE HSIAO, TT TI WORKFORCE CONSIDERATIONS - MAINTENANCE OF THE FUTURE ATC SYSTEM SO PROCEEDINGS OF THE IEEE BP 1766 EP 1775 PG 10 JI Proc. IEEE PY 1989 PD NOV VL 77 IS 11 GA CL319 J9 PROC IEEE UT ISI:A1989CL31900018 PT J AU GOURNIC, J TABAK, D TI AN INTEGRATED DESIGN OF A SATELLITE-BASED NAVIGATION SYSTEM FOR AIR-TRAFFIC CONTROL SO JOURNAL OF MICROCOMPUTER APPLICATIONS BP 267 EP 279 PG 13 JI J. Microcomput. Appl. PY 1989 PD JUL VL 12 IS 3 GA AM595 J9 J MICROCOMPUT APPL UT ISI:A1989AM59500006 PT J AU THACKRAY, RI TOUCHSTONE, RM TI DETECTION EFFICIENCY ON AN AIR-TRAFFIC CONTROL MONITORING TASK WITH AND WITHOUT COMPUTER AIDING SO AVIATION SPACE AND ENVIRONMENTAL MEDICINE BP 744 B-49 EP 748 PG 5 JI Aviat. Space Environ. Med. PY 1989 PD AUG VL 60 IS 8 GA AH856 J9 AVIAT SPACE ENVIRON MED UT ISI:A1989AH85600002 PT J AU COLLINS, WE MERTENS, HW TI AGE, ALCOHOL, AND SIMULATED ALTITUDE - EFFECTS ON PERFORMANCE AND BREATHALYZER SCORES SO AVIATION SPACE AND ENVIRONMENTAL MEDICINE BP 1026 EP 1033 PG 8 JI Aviat. Space Environ. Med. PY 1988 PD NOV VL 59 IS 11 GA Q8414 J9 AVIAT SPACE ENVIRON MED UT ISI:A1988Q841400002 PT J AU COLLINS, WE TI SOME EFFECTS OF SLEEP LOSS ON VESTIBULAR RESPONSES SO AVIATION SPACE AND ENVIRONMENTAL MEDICINE BP 523 EP 529 PG 7 JI Aviat. Space Environ. Med. PY 1988 PD JUN VL 59 IS 6 GA N6374
Page 1 and 2: PsycINFO TY - JOUR ID - 2001-00614-
Page 3 and 4: workload and motion sickness during
Page 5 and 6: training, the Os' height from the g
Page 7 and 8: A1 - Johnson, David M. A1 - Stewart
Page 9 and 10: N2 - Investigated the relationship
Page 11 and 12: uniforms in a UH-60 helicopter simu
Page 13 and 14: design mysteries of hyper-complex o
Page 15 and 16: These were Royal Air Force and Turk
Page 17 and 18: N2 - Investigated the potential mea
Page 19 and 20: KW - Job Performance KW - Work Load
Page 21 and 22: A1 - Oser, Randall L. A1 - Prince,
Page 23 and 24: eserved) KW - Auditory Stimulation
Page 25 and 26: KW - Visual Perception PB - Academi
Page 27 and 28: modifier symbols, such as a nearby
Page 29 and 30: VL - 17 IS - 1 SP - 68-74 PB - Psyc
Page 31 and 32: (PsycINFO Database Record (c) 2000
Page 33 and 34: A1 - Martin, B. A1 - Harlay, F. Y1
Page 35 and 36: KW - Reaction Time KW - fatigue res
Page 37 and 38: AD - U Virginia TY - JOUR ID - 1978
Page 39 and 40: and sea-based operations, and some
Page 41 and 42: Science Citation PT J AU Mertens, H
Page 43 and 44: JI Aerosp. Am. PY 1996 PD JUN VL 34
Page 45 and 46: PT J AU STERN, JA BOYER, D SCHROEDE
Page 47: VL 62 IS 3 GA EZ171 J9 AVIAT SPACE
Page 51 and 52: AU MERTENS, HW BOONE, JO TI FUNCTIO
Page 53 and 54: BP 47 EP 62 PG 16 JI Comput PY 1987
Page 55 and 56: PT J AU DARK, SJ TI MEDICALLY DISQU
Page 57 and 58: PT J AU VANDEVENTER, AD TI A FOLLOW
Page 59 and 60: PG 8 JI Aviat. Space Environ. Med.
Page 61 and 62: significantly differ from normal, w
Page 63 and 64: visual-scene background affected pi
Page 65 and 66: PT J AU Schroeder, JA Chung, WWY TI
Page 67 and 68: BP 35 EP 42 PG 8 JI IEEE Eng. Med.
Page 69 and 70: predictor was also evaluated; at th
Page 71 and 72: flying qualities, using maritime he
Page 73 and 74: WOODSON WE, 1992, HUMAN FACTORS DES
Page 75 and 76: AB Introduction: Night Vision Devic
Page 77 and 78: GOWER DW, 8925 USAARL KNAPP CJ, 199
Page 79 and 80: KENNEDY RS, 1996, HUMAN FACTORS SAF
Page 81 and 82: WARREN WH, 1988, NATURE, V336, P162
Page 83 and 84: MUSTARD BE, 1987, EXP BRAIN RES, V6
Page 85 and 86: J9 J AMER HELICOPTER SOC UT ISI:A19
Page 87 and 88: knowledge bases of tasks, to make t
Page 89 and 90: questions and studies, indicating t
Page 91 and 92: influence of two embedded training
Page 93 and 94: 1988, ELASTIC WRINKLING SA, PS17 19
Page 95 and 96: WARWICK G, 1990, FLIGHT INT, V137,
Page 97 and 98: PD DEC VL 85 IS 12 GA KA952 J9 J RO
Page 99 and 100:
SANDERS MG, 1976, AVIAT SPACE ENV M
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UT ISI:A1990EE34300003 PT J AU SCHR
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KRETSIS G, 1987, THESIS U LONDON EN
Page 105 and 106:
NR 58 CR *N ATL TREAT ORG, 1972, AG
Page 107 and 108:
EP 572 PG 8 JI Hum. Factors PY 1984
Page 109 and 110:
the flight envelope boundaries with
Page 111 and 112:
eliminating the huge losses associa
Page 113 and 114:
novel scanning antenna, with resolu
Page 115 and 116:
Langley plot method and by intercom
Page 117 and 118:
A personal computer-based aviation
Page 119 and 120:
Day/Night Advanced Pilotage System,
Page 121 and 122:
Journal Long Form, 56, Ellerbrock,
Page 123 and 124:
Journal Long Form, 66, Smeyne, Alan
Page 125 and 126:
a manner similar to shape functions
Page 127 and 128:
Journal Long Form, 84, Venkatesan,
Page 129 and 130:
Military cockpits Air to ground tar
Page 131 and 132:
Conference Proceeding, 100, Leacock
Page 133 and 134:
helicopter as well as in a lower ra
Page 135 and 136:
employed visual simulation technolo
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ehavior, goal-processing activities
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completely set up by user in advanc
Page 141 and 142:
Geo/Cockpit Reference display produ
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Smart Structures and Materials 1996
Page 145 and 146:
avoidance data using on-board measu
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helicopters. Subsequent flight test
Page 149 and 150:
improvement had to come from the on
Page 151 and 152:
Annual Forum. Part 1 (of 3), May 9-
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on various rotorcraft motion constr
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DLR realizes flight testing under t
Page 157 and 158:
algorithms are presented. Visual ta
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stabilization, Synthetic Vision for
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wing aircraft where weight is of pa
Page 163 and 164:
The reduction of the minimum altitu
Page 165 and 166:
provided substantial improvements i
Page 167 and 168:
Honeywell has conducted a series of
Page 169 and 170:
analyzed using results which demons
Page 171 and 172:
Journal Long Form, 32, Cagley, Jame
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STD-1553 serial bus. Real-time calc
Page 175 and 176:
imagery at rates varying from five
Page 177 and 178:
Fuzzy logic controllers Genetic alg
Page 179 and 180:
Conference Proceeding, 73, Hansford
Page 181 and 182:
Journal Long Form, 81, Wilkins, Rob
Page 183 and 184:
A new flight research vehicle, the
Page 185 and 186:
employing game theory. Recently, th
Page 187 and 188:
Apr 26-30 1992, Las Vegas, NV, USA
Page 189 and 190:
programming tapes for machines on t
Page 191 and 192:
Proceedings, May 1991, Phoenix, AZ,
Page 193 and 194:
discernible. The control response t
Page 195 and 196:
control logic is designed to accomp
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advances in this field are also dis
Page 199 and 200:
Conference Proceeding, 37, Stringer
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systems is the weight savings resul
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of two rows of three-abreast seatin
Page 205 and 206:
In the main, operating companies of
Page 207 and 208:
An experimental program, which comb
Page 209 and 210:
Conference Proceeding, 30, Ganesan,
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Conference Proceeding, 41, Davis, T
Page 213 and 214:
Conference Proceeding, 52, McCauley
Page 215 and 216:
mode shapes, which are suitable for
Page 217 and 218:
Society. St Louis, MO, USA, America
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Conference Proceeding, 124, Clark,
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SP - 5E5/1-9 vol.2 CY - Piscataway,
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small business innovative research
Page 225 and 226:
standard personal ventilator. While
Page 227 and 228:
JA - Sensor Data Fusion and Integra
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etween the first solo night and pri
Page 231 and 232:
KW - system design KW - display inf
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ID - 6120812 T1 - Flight testing of
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Several new tests are included: an
Page 237 and 238:
SN - 0277-786X AD - Anacapa Sci. In
Page 239 and 240:
N1 - Enhanced and Synthetic Vision
Page 241 and 242:
KW - hover task KW - fixed-based he
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KW - elevation KW - compensation st
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sizes and types will elicit varying
Page 247 and 248:
SP - 95-9 vol.1 CY - Santa Monica,
Page 249 and 250:
ased upon a relatively straightforw
Page 251 and 252:
ID - 5609550 T1 - Rotorcraft safety
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N1 - Braunschweig, Germany N1 - 22-
Page 255 and 256:
KW - overlap binocular field-of-vie
Page 257 and 258:
A1 - Halmos, Z. Y1 - 1995 N1 - Helm
Page 259 and 260:
N1 - vol.2 N1 - Nashville, TN, USA
Page 261 and 262:
KW - optical density KW - optical f
Page 263 and 264:
KW - context-sensitive advice KW -
Page 265 and 266:
N1 - Proceedings of NAECON '93 - Na
Page 267 and 268:
information processing capability t
Page 269 and 270:
A1 - Ahmad, S. Y1 - Jan. 1994 N2 -
Page 271 and 272:
viewing conditions in a rotorcraft
Page 273 and 274:
KW - PC-based Crew Chief Station KW
Page 275 and 276:
A1 - Rash, C. E. A1 - Stephens, R.
Page 277 and 278:
KW - statistical analysis KW - flig
Page 279 and 280:
AD - Westland Helicopters Ltd, Yeov
Page 281 and 282:
judgments and long-term stereo expo
Page 283 and 284:
T1 - Quantitative method for relati
Page 285 and 286:
KW - safety KW - military aviation
Page 287 and 288:
KW - Assistant Air Administrator KW
Page 289 and 290:
KW - response time JA - Proceedings
Page 291 and 292:
forward looking infra-red (FLIR) or
Page 293 and 294:
N1 - Atlanta, GA, USA N1 - 15-17 Ju
Page 295 and 296:
KW - computer-aided engineering KW
Page 297 and 298:
factors) Y1 - June 1987 N2 - The im
Page 299 and 300:
SN - 0852963351 AD - R. Aircraft Es
Page 301 and 302:
KW - cognitively appropriate semant
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TY - CONF ID - 2112021 T1 - Airspee
Page 305 and 306:
CY - New York, NY, USA PB - IEEE AD
Page 307 and 308:
KW - DSAL JA - IEEE PLANS 80. Posit
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KW - operational helicopter aviatio
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N2 - A fixed-base helicopter simula
Page 313 and 314:
fourth-order system, it is applicab
Page 315 and 316:
CS- Lawrence Erlbaum Associates, In
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TRANSPORT AIRCRAFT HUMAN FACTORS IN
Page 319 and 320:
Manufacturing Process and Control T
Page 321 and 322:
AB- This report presents 4 studies.
Page 323 and 324:
SF- MRIS M RN- CG-D-14-90 R&DC 08/9
Page 325 and 326:
ELECTROMAGNETIC INTERFERENCE STORMS
Page 327 and 328:
DE- HELICOPTERS PILOTS (PERSONNEL)
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year of operation. The helicopter c
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CS- Systems Control Technology, Inc
Page 333 and 334:
AU- Treiterer, J PY- 1972 LA- Engli
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PY- 1973 LA- English SF- HRIS H PG-
Page 337 and 338:
SHOWN BY THE FACT THAT THE PERCENTA
Page 339 and 340:
AU- Hess, RA PY- 1977 LA- English S
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PD- 19761000 AU- Clarke, MJ Osborne
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AIRCRAFT ROAD CONSTRUCTION PUBLIC T
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AZ- 2189882 AA- ADA385583/XAB TI-
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TI- Technical rept AU- Berner, W.
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CS- 117341000; 436297 RN- MTI20.97
Page 351 and 352:
order to develop tailored intervent
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encompassed all Class A accidents i
Page 355 and 356:
SH- 92A (Behavior and Society--Job
Page 357 and 358:
Characteristics of the CEP have bee
Page 359 and 360:
LA- English PC- PC A05/MF A01 JA- G
Page 361 and 362:
the mission planning process for th
Page 363 and 364:
AZ- 2116725 AA- N19990009997/XAB T
Page 365 and 366:
was a container express box (CONEX)
Page 367 and 368:
NT- Order this product from NTIS by
Page 369 and 370:
the similarity between two scan pat
Page 371 and 372:
SH- 51C (Aeronautics and Aerodynami
Page 373 and 374:
allowable seat stroking distances (
Page 375 and 376:
CS- 114856001; 434430 RN- AFRL-HE-
Page 377 and 378:
PG- 73p NT- Product reproduced from
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DE- *Spatial distribution; *Visual
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AB- Helmet mounted displays (HMDs)
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from HFI applications on a non-majo
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CP- United States AB- A systematic
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phone at 1-800-553-NTIS (U.S. custo
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helicopter back pain. Based on this
Page 391 and 392:
helicopter simulator. Sixteen non-U
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PY- Mar 97 PG- 50-250 citations NT-
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AA- AD-B095 681/3 TI- Data Present
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CS- 008124000; 234450 RN- ARO/FRI/
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AZ- 1980700 AA- AD-A313 889/8 TI-
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AZ- 1972361 AA- N96-27964/1 TI- Fl
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engineering; Commuter aircraft; Cyb
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RN- TR-1313-1; WL-TR-96-3028 CN- F3
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(Military Sciences--General); 92A (
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Springfield, VA, 22161, USA. LA- En
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SH- 79G (Ordnance--Guns) AZ- 193953
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Flight Crew Perceptions CS- Bioneti
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PY- 1 Sep 95 PG- 38p NT- Order this
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AA- AD-A298 780/8 TI- Video Method
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DE- *Laser target designators; *Pro
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Certification of Advanced Aviation
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PY- cJan 95 PG- 10p NT- In AGARD, L
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PY- Dec 94 PG- 54p NT- Order this p
Page 427 and 428:
LA- English DT- Journal article PC-
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Technology and Human Factors Engine
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PY- Nov 94 PG- 35p NT- Order this p
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eferred to as the Two-Step Method (
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AA- AD-A285 654/0 TI- Laboratory a
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structural loads. (orig.). (Copyrig
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Page 441 and 442:
its basic stability augmentation sy
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flight operations. Both research ef
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environmental and electromagnetic i
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agreed that despite the limitations
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AZ- 1802115 AA- AD-A277 668/0 TI-
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AA- AD-A275 887/8 TI- Vision Impai
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AU- Blair, J. CS- SCIENTECH, Inc.,
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e given to parking clearance criter
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principles relate to the use and fu
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AZ- 1771155 AA- N94-13310/5 TI- Im
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AU- Green, D. L. ; Hart, J. ; Hwosc
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PC- PC A04/MF A01 JA- GRAI9324 CP-
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LA- English PC- (Order as N93-30673
Page 469 and 470:
AB- Established in 1981, the Center
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AU- McAnulty, D. M. ; Ruffner, J. W
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PC- PC A04/MF A01 JA- GRAI9315 CP-
Page 475 and 476:
CP- United Kingdom AB- The ominous
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PG- 20p NT- Previously Announced in
Page 479 and 480:
evacuation; Temperature; Signs and
Page 481 and 482:
Monitor, Model 506 TI- Final rept
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TI- Evaluation of Night Vision Gogg
Page 485 and 486:
AZ- 1691627 AA- AD-A256 245/2 TI-
Page 487 and 488:
Page 489 and 490:
Executive) in the United Kingdom. T
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evaluation, aeromedical equipment.
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Methane; Monitoring; Remote Sensing
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JA- GRAI9223; STAR3020 CP- United S
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available. Success in automating NO
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AA- AD-A251 077/4 TI- Test and Eva
Page 501 and 502:
customers); (703)605-6000 (other co
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de Vision Nocturne) Held in Pensaco
Page 505 and 506:
Operations. The tests were conducte
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Lateral range curves and sweep widt
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airframe spin data is unavailable h
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AZ- 1616136 AA- DE91018195 TI- Rad
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CP- United Kingdom AB- The United K
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The procedures were: ear-canal meas
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PG- 3p NT- In NASA, Washington, 4TH
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CS- 090678000; SP- Sypher:Mueller
Page 521 and 522:
; Vision; Comfort; Flight clothing;
Page 523 and 524:
helmet-mounted display. The experim
Page 525 and 526:
Information und Dokumentation. CS-
Page 527 and 528:
DE- Aeronautics; Altitude; Army res
Page 529 and 530:
their helicopters. Upon selection o
Page 531 and 532:
analysis procedures. DE- *Atropine;
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The data presented will include qua
Page 535 and 536:
SH- 95G (Biomedical Technology and
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DT- Conference proceeding PC- PC A0
Page 539 and 540:
simultaneously improving the signal
Page 541 and 542:
CS- Construction Engineering Resear
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engine and transmission data at all
Page 545 and 546:
CS- Advisory Group for Aerospace Re
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satisfies these requirements and in
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performance ID- *Foreign technology
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PG- 445p NT- Product reproduced fro
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LA- English DT- Conference proceedi
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Page 557 and 558:
to military standards by the U.S. A
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AH1FWS to deficiencies in the visua
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AZ- 1469342 AA- PB90-850959 TI- Mi
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to provide near compatible solution
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AA- PB89-867261 TI- Head Up Displa
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and feasibility study was performed
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AZ- 1434792 AA- N89-17579/8 TI- Ti
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clothing; Thermal properties ID- *F
Page 573 and 574:
technique, in terms of learned cont
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augmentation; Workloads (Psychophys
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PG- 57p NT- In German, With 12 refs
Page 579 and 580:
CP- United States AB- There has bee
Page 581 and 582:
CN- N00014-84-C-2442 PY- 1 Oct 88 P
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vehicle. Evaluations of the integra
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(Electrotechnology--Optoelectronic
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performed maximal voluntary exertio
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AZ- 1362979 AA- N88-16653/3 TI- In
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PC- PC A25/MF A01 JA- GRAI8812; STA
Page 593 and 594:
ID- NTISNASA SH- 51F (Aeronautics a
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Questionnaires; Rates; Recognition;
Page 597 and 598:
y sideslip, and some effective dihe
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Page 601 and 602:
CS- 019045001; NC473657 RN- NAS 1.
Page 603 and 604:
DE- *Spinal column; *Posture(Physio
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for point sources and from 1 to 200
Page 607 and 608:
AA- N87-14304/6 TI- Emergency Exit
Page 609 and 610:
Cockpits; Day; Dynamics; Flight; Hi
Page 611 and 612:
affected by helicopter vibration. D
Page 613 and 614:
for the analysis of pilot workload
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factors engineering; *Man machine s
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CP- United States AB- This paper di
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email at orders@ntis.fedworld.gov.
Page 621 and 622:
aircraft; Lightweight; Management;
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Road, Springfield, VA, 22161, USA.
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AB- Thirteen subanalyses were perfo
Page 627 and 628:
Directly related functions included
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integrated avionics system with the
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AA- N85-25237/7 TI- Rotorcraft Dig
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AB- No abstract available. DE- *Coc
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control, which encompasses the area
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Pollution and Control) AZ- 1146347
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AB- The operational, technical, and
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AU- Chaffin, W. ; Hiott, B. F. ; Kn
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for helicopters engaged in low-leve
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CP- United States AB- The U.S. Navy
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AA- AD-P002 708/6 TI- Army Helicop
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PG- 25p NT- In Dutch; English Summa
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and Propellants--Jet and Gas Turbin
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AZ- 1057954 AA- AD-P001 626/1 TI-
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engineering, Flight control systems
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1-800-553-NTIS (U.S. customers); (7
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ID- Color display systems; F-16 air
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SP- National Aeronautics and Space
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addressed. DE- *Aeronautical engine
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ID- Nap of the Earth; JUH-1H aircra
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CS- 026909000; 404578 RN- USAARL-8
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SH- 51B (Aeronautics and Aerodynami
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TI- Final Report AU- Rue, R. J. ;
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Aerodynamics--Avionics) AZ- 0972179
Page 693 and 694:
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LA- English PC- MF A01 JA- GRAI8219
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aviation operations is presented. T
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NT- Workshop Held at Palo Alto, Cal
Page 701 and 702:
TI- Airworthiness and Flight Charac
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CS- Aeronautical Research Labs., Me
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of 1978-1979 (Anderson and Jahnsen,
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DE- *Cockpits; *Display systems; In
Page 709 and 710:
Field intensity; Electric fields; P
Page 711 and 712:
of conventional electrical cable (s
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; *Nasa programs; *Policies; *Resea
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UH-60A. Early in the UTTAS conceptu
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the frequency range of 40 to 1000 H
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*Aviation safety; NATO; Low tempera
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LA- English PC- PC A02/MF A01 JA- G
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CS- Army Aeromedical Research Lab.,
Page 729 and 730:
PG- 48p NT- See also Volume 9, AD-A
Page 731 and 732:
AZ- 0854718 AA- AD-A089 191/1/XAB
Page 733 and 734:
his vision by special displays so a
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Springfield, VA. NT- Order this pro
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long-term technologies into an adva
Page 739 and 740:
PY- 24 Mar 80 PG- 16p NT- Trans. of
Page 741 and 742:
PY- Feb 80 PG- 55p NT- Order this p
Page 743 and 744:
presents the facts, conditions, cir
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AU- Robertson, D. G. CS- Department
Page 747 and 748:
Page 749 and 750:
AZ- 0792294 AA- N79-32834/0/XAB TI
Page 751 and 752:
Page 753 and 754:
attention inside the cockpit. (Auth
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Page 757 and 758:
Flight crews; Fatigue; Human factor
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discussions. The data collected ind
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(Communication--Verbal) AZ- 0734790
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accuracy of theoretical flow field
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RN- USAARL-SPECIAL BIB-SER-9-SUP-1
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AB- The results of test programs co
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Charge/Detonation System; Dice Thro
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sensors, a cooling generator, and a
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at (703)321-8547; and email at orde
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Page 777 and 778:
information content was entirely de
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CN- NONR414800 PY- Feb 65 PG- 64p N
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toxicology evaluation are continuin
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NT- Distribution limitation now rem
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is more effective than either of th
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PC- PC A06/MF A01 JA- GRAI7710 AB-
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countries); fax at (703)321-8547; a
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AB- The objective of the program is
Page 795 and 796:
Requirements, Analysis of R and D T
Page 797 and 798:
Page 799 and 800:
at various wind azimuths were inves
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NT- See also Study 2, AD-A007 812.
Page 803 and 804:
AZ- 0588820 AA- AD-A032 028/3/XAB
Page 805 and 806:
CS- Army Scientific Advisory Panel
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SH- 51B (Aeronautics and Aerodynami
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AZ- 0577573 AA- AD-871 350/5/XAB T
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NT- Distribution limitation now rem
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PY- Nov 70 PG- 190p NT- Distributio
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(Ordnance--Guns) AZ- 0570727 AA- A
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AZ- 0569991 AA- AD-923 214/1/XAB T
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AB- The expanded service test of th
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Calibration ID- *Uh-1n aircraft; Ca
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CS- 332500 CN- DAHC19-71-C-0021; S
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AZ- 0567498 AA- AD-881 186/1/XAB T
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SH- 68B (Environmental Pollution an
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controlling the airspeed of a helic
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Considerations TI- Final rept. 30
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from flight test data. The programs
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supplies, and sample transcripts of
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DE- *Microphones; *Noise reduction;
Page 845 and 846:
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CS- Army Materiel Command Texarkana
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assigning the crews for the field t
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tracking, parachutes, balloon telem
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oute structure in the New York area
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SH- 74E (Military Sciences--Logisti
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during April and June 1973. (Author
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AZ- 0456286 AA- N74-27504/1/XAB TI
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the criteria values. (Author) DE- *
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claims. Most all the projects on wa
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PC- PC A07/MF A01 JA- GRAI7408 AB-
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AB- The report describes POBAL, a t
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JA- GRAI7319 AB- A higher harmonic
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AB- Three experiments designed to d
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AA- AD-751 217/XAB TI- High Perfor
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SH- 92B (Behavior and Society--Psyc
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DE- *Pilots; *Visual perception; *H
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AZ- 0297921 AA- AD-733 671/XAB TI-
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of VTOL aircraft and helicopters. A
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Development--Emergency Services and
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ID- C-142 aircraft; Gust alleviatio
Page 887 and 888:
Page 889 and 890:
conducted at Edwards Air Force Base
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PY- 1969 PG- 135p NT- Proceedings o
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helicopter and second the effect th
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AZ- 0190814 AA- AD-691 299/XAB TI-
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AZ- 0182500 AA- N69-21707/XAB TI-
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CS- 142925 RN- TR-1-214-VOL-1; HS-
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PY- Feb 68 PG- 30p NT- Order this p
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multivariable vehicular control sys
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Tandem Rotor Helicopter. Volume I.
Page 909 and 910:
ecommendation that no tinted media
Page 911 and 912:
TI- Technical rept CS- Aviation Sa
Page 913 and 914:
schemes, applied to the main rotor
Page 915 and 916:
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situation. (Author) DE- *Aviation p
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RN- JANAIR-TR-D228-100-011 CN- NONR
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een completed. From the information
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TI- State of the ART for V/STOL Con
Page 925 and 926:
fixed-wind flyable system and two r
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AA- AD-602 125/XAB TI- Helicopter
Page 929 and 930:
tunnel models; Model tests; Take-of
Page 931 and 932:
support, and internal situational a
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including NVG and HMD are offered w
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AN- 02559555 AN- A01-17563 TI- Fi
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SH- 7554 Man/System Technology & Li
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TI- Evaluation of algorithms for fu
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AN- 02535822 AN- A00-46831 TI- Ca
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TI- Evaluation of a motion fidelity
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REFUELING; PERSONAL COMPUTERS; ALGO
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PD- 199900 RF- 18 LA- English GL- G
Page 949 and 950:
technology is currently available t
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situation is always unique and ther
Page 953 and 954:
total rate of 0.22 accidents per 10
Page 955 and 956:
least one environmental test. Ninet
Page 957 and 958:
order to recommend improvements in
Page 959 and 960:
Operations by Enhanced Training AU-
Page 961 and 962:
AN- A00-26130 TI- The effects of p
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GL- United States CP- United States
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AN- A99-40429 TI- Helmet-mounted d
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were analyzed using frequency domai
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missions. The development, integrat
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involving heavy machinery (e.g., mu
Page 973 and 974:
PD- 199900 LA- English GL- United S
Page 975 and 976:
The increasingly important topic of
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RN- NASA no. 19990025678 LA- Englis
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RN- NASA no. 19980218991 LA- Englis
Page 981 and 982:
communication system. Sixteen air t
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A stepwise multiple regression foun
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partial restoration of recordings b
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DE- HUMAN FACTORS ENGINEERING; IN-F
Page 989 and 990:
own recollections and involvement i
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displays in lieu of miniaturized CR
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SH- 7581 Administration & Managemen
Page 995 and 996:
AN- 02347126 AN- A98-27588 TI- An
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licence of the MiG-15 jet fighter a
Page 999 and 1000:
Alexandria, VA, American Helicopter
Page 1001 and 1002:
increase at the high rates typical
Page 1003 and 1004:
LA- English GL- United States CP- U
Page 1005 and 1006:
DE- WORKLOADS (PSYCHOPHYSIOLOGY); A
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the ANR system on, and, with and wi
Page 1009 and 1010:
JA- STAR9701 AB- Rotorcraft-pilot c
Page 1011 and 1012:
AN- 02315521 AN- A97-41062 TI- An
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DE- HARDWARE; PERFORMANCE TESTS; FL
Page 1017 and 1018:
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weaknesses relative to the harness
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AN- 02292483 AN- N97-10549 TI- Vi
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AV- CASI HC A03/MF A04 JA- STAR961
Page 1025 and 1026:
manufacturers, research institution
Page 1027 and 1028:
SH- 7503 Air Transportation & Safet
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AB- There is a need for calibrated
Page 1031 and 1032:
helicopters of different weight (li
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JA- IAA9612 AB- Indonesian Air Forc
Page 1035 and 1036:
AN- 02259646 AN- A96-44927 TI- De
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SO- In: Laser radar technology and
Page 1039 and 1040:
favorable alternative to the 'norma
Page 1041 and 1042:
CP- United States DT- CONFERENCE PR
Page 1043 and 1044:
instrumented Cobra helicopter. The
Page 1045 and 1046:
Page 1047 and 1048:
participated. Using a UH-60 flight
Page 1049 and 1050:
TRACKING; *MARINE METEOROLOGY; *MET
Page 1051 and 1052:
various size and gender aircrew usi
Page 1053 and 1054:
etween flight performance with and
Page 1055 and 1056:
PD- 199300 RF- 10 CN- NAG2-308 LA-
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SH- 7508 Aircraft Stability & Contr
Page 1059 and 1060:
JAS 39 cockpit display system, impr
Page 1061 and 1062:
SO- In: AHS, Annual Forum, 51st, Fo
Page 1063 and 1064:
AB- The technical approach for the
Page 1065 and 1066:
instrumentation system was designed
Page 1067 and 1068:
Page 1069 and 1070:
esults are presented in this paper.
Page 1071 and 1072:
AU- MULDER, J. A. (Technische Univ.
Page 1073 and 1074:
AU- Cadogan, David P.; Jackson, Lis
Page 1075 and 1076:
AN- A95-22480 TI- Helicopter noise
Page 1077 and 1078:
SO- In: AHS, Annual Forum, 50th, Wa
Page 1079 and 1080:
Page 1081 and 1082:
DE- *FLIGHT OPERATIONS; *FLIGHT SA
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DT- CONFERENCE PAPER AV- AIAA Tech
Page 1085 and 1086:
involved a delay of rise times afte
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DE- *AIRCRAFT PILOTS; *HELICOPTERS
Page 1089 and 1090:
intermittently. Instructions in Exp
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SO- In: AHS, Annual Forum, 49th, Sa
Page 1093 and 1094:
AN- 02128051 AN- A94-19165 TI- Ev
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PD- 199300 RF- 6 LA- English GL- Un
Page 1097 and 1098:
TI- Flight tests of the digitally c
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CP- United States DT- REPORT AV- A
Page 1101 and 1102:
Furthermore, we will focus on the s
Page 1103 and 1104:
measures experimental design. The r
Page 1105 and 1106:
AN- 02101511 AN- N93-15016 TI- Tr
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INTENSITY; *NOISE REDUCTION DE- AER
Page 1109 and 1110:
to simulating motion effects on sin
Page 1111 and 1112:
AN- 02077830 AN- A93-37878 TI- Di
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AB- Tests conducted on a variety of
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SH- 7506 Aircraft Instrumentation (
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AU- VOLODKO, A. M.; VERKHOZIN, M. P
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professional'nuiu nadezhnost' letch
Page 1121 and 1122:
ecent sea trials are examined. (Aut
Page 1123 and 1124:
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AN- 02032965 AN- N92-17165 TI- Sy
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AN- 02027444 AN- N92-11629 TI- Pe
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FLIGHT; *VISUAL SIGNALS DE- FLIGHT
Page 1131 and 1132:
that a steep 'trans-cockpit authori
Page 1133 and 1134:
DE- *BEARING (DIRECTION); *HELICOP
Page 1135 and 1136:
autogiro are described. The work wa
Page 1137 and 1138:
AV- AIAA Technical Library JA- IAA
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AN- 01984386 AN- A92-16050 TI- Fl
Page 1141 and 1142:
and convenient means of acquiring t
Page 1143 and 1144:
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DE- *ANTHROPOMETRY; *HELICOPTER PE
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AN- N91-29730 TI- Performance of s
Page 1149 and 1150:
a contact lens. Up-to-date results
Page 1151 and 1152:
trainability of aspirant pilots to
Page 1153 and 1154:
Subsequent changes in cockpit WBGT
Page 1155 and 1156:
PY- 1990 PD- 199010 RF- 11 RN- SAE
Page 1157 and 1158:
AN- 01929682 AN- A91-31295 TI- NA
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SN- 0360-5450 LA- English GL- Germa
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TESTS; FRACTURE MECHANICS; HUMAN FA
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DE- *AH-64 HELICOPTER; *AVIONICS;
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RN- AIAA PAPER 90-3172 LA- English
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SH- 1C Aircraft SH- 7508 Aircraft
Page 1169 and 1170:
NT- Prepared in cooperation with Fe
Page 1171 and 1172:
Symbology Tutor, consists of an int
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SN- 0091-3286 LA- English GL- Unite
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AN- 01877767 AN- A90-42495 TI- He
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HELICOPTER TAIL ROTORS; HIGH STRENG
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attention. The different assumption
Page 1181 and 1182:
SH- 7506 Aircraft Instrumentation (
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DE- *CONTROL SYSTEMS DESIGN; *FLIG
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AN- 01863439 AN- A90-28167 TI- HA
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CP- United States DT- CONFERENCE PA
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AN- 01854825 AN- A90-19553 TI- Si
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approach, a control aid program ope
Page 1193 and 1194:
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SO- IN: AIAA Flight Simulation Tech
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of modern military helicopters are
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analyzed for content, agencies invo
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DT- PREPRINT AV- AIAA Technical Li
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tilt-rotor aircraft, as derived fro
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ecently implemented OH-6A helicopte
Page 1207 and 1208:
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AU- FITZPATRICK, DANIEL T. (Hawaii,
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DT- REPORT AV- AIAA Technical Libr
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AB- The National Transportation Saf
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AN- A88-53659 TI- Determination of
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*NAVIGATION INSTRUMENTS; *VIDEO EQU
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PD- 198700 RF- 23 LA- English GL- U
Page 1221 and 1222:
JA- IAA8817 AB- One- and two-person
Page 1223 and 1224:
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development of turbines, ramjet eng
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(STAR) aircraft. The STAR, a one-of
Page 1229 and 1230:
AU- PELEGRIN, MARC J. (ONERA, Centr
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DE- ATTITUDE CONTROL; CONTROL SIMUL
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NT- Colloquium held in Brunswick, W
Page 1235 and 1236:
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AB- The prevalence of backache amon
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AB- Helicopter pilots were used to
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sizes and distances in the visual s
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*FLIGHT TESTS; *MANUAL CONTROL; *ME
Page 1245 and 1246:
SF- DTIC DE- *ANTIEMETICS AND ANTI
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DE- *CONFERENCES; *FLIGHT SIMULATI
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GL- United Kingdom CP- Germany DT-
Page 1251 and 1252:
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SH- 7505 Aircraft Design, Testing &
Page 1255 and 1256:
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JA- IAA8713 AB- A topographic map a
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personnel and, in the long run, in
Page 1261 and 1262:
AN- 01636068 AN- A87-19255 TI- Fl
Page 1263 and 1264:
systems. An important feature of th
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PD- 198500 RF- 287 LA- Russian GL-
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DE- CONTROL STABILITY; FEEDBACK CON
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GL- Germany CP- Germany DT- CONFERE
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TI- The T800 turbine engine solicit
Page 1273 and 1274:
variation in scene content and text
Page 1275 and 1276:
TI- Helicopter flight control with
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Black Hawk. The program phases incl
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LA- English GL- Australia CP- Unite
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AN- 01602456 AN- A86-26004 TI- AI
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AN- 01600170 AN- A86-23718 TI- Re
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flight, and a requirement for the p
Page 1287 and 1288:
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AN- 01590810 AN- A86-14356 TI- Th
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GL- Germany CP- International Organ
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SH- 7599 General (1975-) AN- 01570
Page 1295 and 1296:
AU- COYLE, S. CS- Aerospace Enginee
Page 1297 and 1298:
SH- 5H Man-machine Relations SH- 7
Page 1299 and 1300:
PERFORMANCE; *TASKS DE- FEEDBACK CO
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DE- NOISE MEASUREMENT; NOISE PREDIC
Page 1303 and 1304:
against the stressors found in all
Page 1305 and 1306:
DE- AIRFRAMES; FLIGHT TESTS; HIGH S
Page 1307 and 1308:
and test procedures; a battery of 1
Page 1309 and 1310:
AU- EYRAUD, M. Y.; BOROWSKY, M. S.
Page 1311 and 1312:
pilot eyes-down time, and 100 perce
Page 1313 and 1314:
Page 1315 and 1316:
of the Fourteenth Annual Symposium,
Page 1317 and 1318:
Page 1319 and 1320:
DE- *AIRCRAFT DESIGN; *AVIONICS; *
Page 1321 and 1322:
access the results data base on-lin
Page 1323 and 1324:
DE- AIRLINE OPERATIONS; ALTITUDE SI
Page 1325 and 1326:
control augmentation system (SCAS),
Page 1327 and 1328:
AU- LAVASSAR, L. J. SO- Cockpit (IS
Page 1329 and 1330:
eplaceable assembly (WRA) which, ut
Page 1331 and 1332:
TI- Backache in Chetak crew and sug
Page 1333 and 1334:
CP- France DT- PREPRINT AV- AIAA T
Page 1335 and 1336:
symbols superimposed upon terrain-b
Page 1337 and 1338:
CP- United States DT- CONFERENCE PA
Page 1339 and 1340:
SH- 7501 Aeronautics--General (1975
Page 1341 and 1342:
CS- LB799994 PY- 1982 PD- 198210 N
Page 1343 and 1344:
AN- 01431976 AN- N83-13059 TI- Ae
Page 1345 and 1346:
LA- English GL- U.S.S.R. CP- United
Page 1347 and 1348:
DE- *AIRCRAFT INSTRUMENTS; *DATA A
Page 1349 and 1350:
considered include: (1) separation
Page 1351 and 1352:
HORIZONTAL FLIGHT; PHYSIOLOGICAL FA
Page 1353 and 1354:
model or is the new model to be pro
Page 1355 and 1356:
CS- Centre d'Etudes et de Recherche
Page 1357 and 1358:
efficient and cost effective data t
Page 1359 and 1360:
HELICOPTERS SH- 7504 Aircraft Commu
Page 1361 and 1362:
RF- 44 LA- French GL- France CP- Fr
Page 1363 and 1364:
of instrumentation, palm rests were
Page 1365 and 1366:
LA- Russian CP- U.S.S.R. DT- JOURNA
Page 1367 and 1368:
commercial and military aircraft fr
Page 1369 and 1370:
AN- A82-43755 TI- Laser Doppler an
Page 1371 and 1372:
Helicopter Society, 1982, p. 43-54.
Page 1373 and 1374:
an NOE route with significantly mor
Page 1375 and 1376:
Germany, September 16-19, 1980, Rep
Page 1377 and 1378:
y insurance and depreciation, while
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RF- 1 NT- In AGARD Aural Commun. in
Page 1381 and 1382:
addressed. (R.C.T.) SF- NASA CASI D
Page 1383 and 1384:
AU- KRUEGER, G. P.; ARMSTRONG, R. N
Page 1385 and 1386:
RN- AD-A089794; ER-15047; USAAVRADC
Page 1387 and 1388:
CP- International Organization DT-
Page 1389 and 1390:
AV- AIAA Technical Library AV- NT
Page 1391 and 1392:
American Helicopter Society, 1981,
Page 1393 and 1394:
LA- English GL- France CP- United S
Page 1395 and 1396:
Page 1397 and 1398:
DE- *CONTROLLABILITY; *FLIGHT CONT
Page 1399 and 1400:
JA- IAA8116 AB- The optimal control
Page 1401 and 1402:
CP- Netherlands DT- ANALYTIC OF COL
Page 1403 and 1404:
AB- The conference included papers
Page 1405 and 1406:
experiments using a ground-based fl
Page 1407 and 1408:
SH- 7553 Behavioral Science (1975-)
Page 1409 and 1410:
JA- IAA8008 AB- This research was i
Page 1411 and 1412:
AU- CHILDS, J. M. CS- Canyon Resear
Page 1413 and 1414:
PY- 1978 PD- 197811 PG- 63P. CN- EY
Page 1415 and 1416:
is installed; (4) the interior is n
Page 1417 and 1418:
NT- In AGARD Operational Helicopter
Page 1419 and 1420:
discussed. The present injury and f
Page 1421 and 1422:
Page 1423 and 1424:
DE- *AIRCRAFT MANEUVERS; *AIRCRAFT
Page 1425 and 1426:
called CUBITS to establish a single
Page 1427 and 1428:
10-51) LA- English GL- United State
Page 1429 and 1430:
and heading retention was installed
Page 1431 and 1432:
Page 1433 and 1434:
Page 1435 and 1436:
handling tasks. Performance is meas
Page 1437 and 1438:
SH- 7508 Aircraft Stability & Contr
Page 1439 and 1440:
RF- 12 LA- German GL- Germany, Fede
Page 1441 and 1442:
factors, all-weather capability, pa
Page 1443 and 1444:
JA- IAA7905 AB- A human factors eva
Page 1445 and 1446:
AU- KNIGHT, V. H., JR. (NASA, Langl
Page 1447 and 1448:
Page 1449 and 1450:
AV- NTIS HC A17/MF A01 JA- STAR782
Page 1451 and 1452:
AN- N78-26055 TI- Flight performan
Page 1453 and 1454:
DE- *AEROSPACE MEDICINE; *AIRCRAFT
Page 1455 and 1456:
to control column deflection. Headq
Page 1457 and 1458:
mecaniques AU- POIRIER, J. L.; BEAU
Page 1459 and 1460:
AN- 00936713 AN- A78-36948 TI- A
Page 1461 and 1462:
DE- *AIRCRAFT INSTRUMENTS; *BOEING
Page 1463 and 1464:
AB- This paper proposes a design pr
Page 1465 and 1466:
simulated AH-1 mission before and a
Page 1467 and 1468:
Page 1469 and 1470:
generating effectiveness data, and
Page 1471 and 1472:
Page 1473 and 1474:
AB- Aviators were required to fly a
Page 1475 and 1476:
PD- 197509 PG- 30P. CN- DA PROJ. 3A
Page 1477 and 1478:
audio, and oscillograph recording e
Page 1479 and 1480:
(U.S. Army, Avionics Laboratory, Fo
Page 1481 and 1482:
test. (G.R.) SF- AIAA DE- *AVIONIC
Page 1483 and 1484:
voice-transmitted 'check caution pa
Page 1485 and 1486:
148 p PY- 1975 PD- 197500 LA- Engli
Page 1487 and 1488:
AN- 00791646 AN- A76-34165 TI- Cr
Page 1489 and 1490:
vestibular sensory organs (semicirc
Page 1491 and 1492:
TI- Research and development applic
Page 1493 and 1494:
systems has shown that conventional
Page 1495 and 1496:
Page 1497 and 1498:
Page 1499 and 1500:
NT- In AGARD The Guidance and Contr
Page 1501 and 1502:
TI- Proceedings of Conference on Ai
Page 1503 and 1504:
It consists of a simple cross hair
Page 1505 and 1506:
PG- 357P. NT- Transl. into ENGLISH
Page 1507 and 1508:
ENGINEERING SH- 6503 Auxiliary Syst
Page 1509 and 1510:
which have been conducted in an eff
Page 1511 and 1512:
Page 1513 and 1514:
CS- NN881427 PY- 1973 PD- 197308 P
Page 1515 and 1516:
AN- A75-39535 TI- The United State
Page 1517 and 1518:
AN- 00692795 AN- A75-19690 TI- Co
Page 1519 and 1520:
SH- 7552 Aerospace Medicine (1975-)
Page 1521 and 1522:
SF- AIAA DE- *AERODYNAMIC CHARACTE
Page 1523 and 1524:
AB- Review of the experiences and f
Page 1525 and 1526:
'mean' value of pilot ability to pe
Page 1527 and 1528:
DE- AIRSPEED; ANGULAR DISTRIBUTION;
Page 1529 and 1530:
PD- 197302 NT- In AGARD Advanced Ro
Page 1531 and 1532:
Page 1533 and 1534:
DE- *FEEDBACK CONTROL; *MANUAL CON
Page 1535 and 1536:
Page 1537 and 1538:
SH- 5I Personnel Selection, Traini
Page 1539 and 1540:
orientation-error problem in Army a
Page 1541 and 1542:
AB- The philosophy of instruction,
Page 1543 and 1544:
DE- CONFERENCES; PROBABILITY THEORY
Page 1545 and 1546:
SH- 6502 Aircraft (1965-74) AN- 00
Page 1547 and 1548:
PY- 1973 PD- 197309 RF- 5 RN- AIAA
Page 1549 and 1550:
heat shield thermodynamic instrumen
Page 1551 and 1552:
LA- German GL- Germany CP- Germany
Page 1553 and 1554:
Page 1555 and 1556:
JA- IAA7215 AB- Human factor proble
Page 1557 and 1558:
AU- SKUBINNA, E. (Deutsche Forschun
Page 1559 and 1560:
Somerset, England) SO- (British Aco
Page 1561 and 1562:
PY- 1971 PD- 197105 NT- IN DGLR FLI
Page 1563 and 1564:
trainers, helicopter response chara
Page 1565 and 1566:
CP- United States DT- REPORT AV- A
Page 1567 and 1568:
Page 1569 and 1570:
Page 1571 and 1572:
ASTRONAUTICS, AND U. OF TEXAS, JOIN
Page 1573 and 1574:
CP- United States DT- PREPRINT AV-
Page 1575 and 1576:
DE- *EYE MOVEMENTS; *HELICOPTERS;
Page 1577 and 1578:
DE- AIR NAVIGATION; AIRCRAFT SAFETY
Page 1579 and 1580:
CS- George Washington Univ., Alexan
Page 1581 and 1582:
AN- N69-11133 TI- Concept formulat
Page 1583 and 1584:
Page 1585 and 1586:
JA- STAR6809 SF- NASA CASI DE- *EV
Page 1587 and 1588:
*MATHEMATICAL MODELS; *PILOT PERFOR
Page 1589 and 1590:
SH- 6501 Aerodynamics (1965-74) AN-
Page 1591 and 1592:
SF- AIAA DE- *AIRCRAFT STABILITY;
Page 1593 and 1594:
Page 1595 and 1596:
Page 1597 and 1598:
Page 1599 and 1600:
AN- 00214600 AN- N66-16533 TI- Av
Page 1601 and 1602:
Page 1603 and 1604:
AN- N65-21056 TI- Contact analog s
Page 1605 and 1606:
DT- REPORT; CONFERENCE PAPER DT- TR
Page 1607 and 1608:
TI- Effect of helicopter dynamics
Page 1609 and 1610:
DE- *FLICKER; *FLIGHT CREWS; *HELI
Page 1611 and 1612:
addresses the safety issue first fr
Page 1613 and 1614:
p<0.0002). There is a dose-respo
Page 1615 and 1616:
decrements, and (2) fatigue effects
Page 1617 and 1618:
Number of References: 21 Original L
Page 1619 and 1620:
iological experiments that require
Page 1621 and 1622:
Source: IEEE Transactions on System
Page 1623 and 1624:
Classification Number(s): 07-01-00;
Page 1625 and 1626:
Volume: 5 Issue: 2 Pages: 95-112 Nu
Page 1627 and 1628:
which are used in teleoperation and
Page 1629 and 1630:
may also result in an accident. One
Page 1631 and 1632:
Volume: 3 Issue: 3 Pages: 163-176 N
Page 1633 and 1634:
tactical flight is dangerous after
Page 1635 and 1636:
dark focus was measured in pilots (
Page 1637 and 1638:
view, eye relief and exit pupil. Th
Page 1639 and 1640:
Original Language: English Classifi
Page 1641 and 1642:
and the perception of orientation a
Page 1643 and 1644:
etween aircraft roll and pilot head
Page 1645 and 1646:
Pages: 398-402 Number of References
Page 1647 and 1648:
An analysis of U.S. civil aviation
Page 1649 and 1650:
Page 1651 and 1652:
U.S. Coast Guard helicopter pilots
Page 1653 and 1654:
each segment were described. An out
Page 1655 and 1656:
Page 1657 and 1658:
maintenance of force outputs. One c
Page 1659 and 1660:
Issue: - Pages: 240-263 Number of R
Page 1661 and 1662:
esearch and development for helicop
Page 1663 and 1664:
influenced by such factors as the u
Page 1665 and 1666:
Abstract Number: 117454 Title: Revi
Page 1667 and 1668:
Volume: - Issue: - Pages: 37pp Numb
Page 1669 and 1670:
Volume: - Issue: - Pages: 66-70 Num
Page 1671 and 1672:
mission performance. These results
Page 1673 and 1674:
Title: Training Head Movement in Vi
Page 1675 and 1676:
Classification Number(s): 08-03-00;
Page 1677 and 1678:
Abstract: The potential benefit of
Page 1679 and 1680:
were sometimes flying aircraft duri
Page 1681 and 1682:
Volume: - Issue: - Pages: 209-212 N
Page 1683 and 1684:
and to develop more incisive criter
Page 1685 and 1686:
Source: Designing for the Global Vi
Page 1687 and 1688:
Abstract: In previous research, cha
Page 1689 and 1690:
Source: Speech Communication Year:
Page 1691 and 1692:
Abstract Number: 145856 Title: Nois
Page 1693 and 1694:
Abstract: The U.S. Army Aeromedical
Page 1695 and 1696:
Abstract: Dexedrine (3, 10-mg doses
Page 1697 and 1698:
Classification Term(s): Surveys, st
Page 1699 and 1700:
Issue: 4 Pages: 407-420 Number of R
Page 1701 and 1702:
Source: Progress for People. Procee
Page 1703 and 1704:
Source: Proceedings of the Tenth In
Page 1705 and 1706:
In a world with increasing mobility
Page 1707 and 1708:
Pages: 387-391 Number of References
Page 1709 and 1710:
Page 1711 and 1712:
Number of References: 13 Original L
Page 1713 and 1714:
controller via data link were asses
Page 1715 and 1716:
Abstract Number: 165913 Title: Curr
Page 1717 and 1718:
Author(s): STEIN, E.S.; WILLEMS, B.
Page 1719 and 1720:
Year: 2001 Volume: 11 Issue: 1 Page
Page 1721 and 1722:
Abstract: The management and transf
Page 1723 and 1724:
Source: Designing for Diversity. Pr
Page 1725 and 1726:
Year: 1995 Volume: - Issue: - Pages
Page 1727 and 1728:
identification of specific conditio
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