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EP 6 PG 1 JI IEEE Softw. PY 1995 PD NOV VL 12 IS 6 GA TB597 J9 IEEE SOFTWARE UT ISI:A1995TB59700004 PT J AU EDWARDS, MB FULLER, DK VORTAC, OU MANNING, CA TI THE ROLE OF FLIGHT PROGRESS STRIPS IN EN-ROUTE AIR-TRAFFIC- CONTROL - A TIME-SERIES ANALYSIS SO INTERNATIONAL JOURNAL OF HUMAN-COMPUTER STUDIES BP 1 EP 13 PG 13 JI Int. J. Hum.-Comput. Stud. PY 1995 PD JUL VL 43 IS 1 GA RW278 J9 INT J HUM-COMPUT STUDIES UT ISI:A1995RW27800001 PT J AU VORTAC, OU EDWARDS, MB MANNING, CA TI SEQUENCES OF ACTIONS FOR INDIVIDUAL AND TEAMS OF AIR-TRAFFIC- CONTROLLERS SO HUMAN-COMPUTER INTERACTION BP 319 EP 343 PG 25 JI Hum.-Comput. Interact. B-44 PY 1994 VL 9 IS 3-4 GA QC240 J9 HUMAN-COMPUTER INTERACTION UT ISI:A1994QC24000003 PT J AU RITTER, RD TI PILOT ERROR IN AUTOMATED SYSTEMS SHOWN BY ALTITUDE DEVIATION REPORTS SO IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE BP 15 EP 19 PG 5 JI IEEE Aerosp. Electron. Syst. Mag. PY 1994 PD APR VL 9 IS 4 GA NE469 J9 IEEE AEROSP ELECT SYST MAG UT ISI:A1994NE46900003 PT J AU SALAZAR, GJ TI HYPEROPIC THERMAL KERATOPLASTY PROCEDURE IN A CIVILIAN AIR- TRAFFIC-CONTROLL SO AVIATION SPACE AND ENVIRONMENTAL MEDICINE BP 772 EP 774 PG 3 JI Aviat. Space Environ. Med. PY 1994 PD AUG VL 65 IS 8 GA PA921 J9 AVIAT SPACE ENVIRON MED UT ISI:A1994PA92100015
PT J AU STERN, JA BOYER, D SCHROEDER, D TI BLINK RATE - A POSSIBLE MEASURE OF FATIGUE SO HUMAN FACTORS BP 285 EP 297 PG 13 JI Hum. Factors PY 1994 PD JUN VL 36 IS 2 GA NZ351 J9 HUM FACTORS UT ISI:A1994NZ35100009 PT J AU MOSS, MT SEGAL, HM TI THE EMISSIONS AND DISPERSION MODELING SYSTEM (EDMS) - ITS DEVELOPMENT AND APPLICATION AT AIRPORTS AND AIRBASES SO JOURNAL OF THE AIR & WASTE MANAGEMENT ASSOCIATION BP 787 EP 790 PG 4 JI J. Air Waste Manage. Assoc. PY 1994 PD JUN VL 44 IS 6 GA NR323 J9 J AIR WASTE MANAGE ASSOC UT ISI:A1994NR32300004 PT J AU MALOTKY, LO TI INTRODUCTION TO THE 6TH INTERNATIONAL-CIVIL-AVIATION-SECURITY- CONFERENCE (AVSEC 93) SO JOURNAL OF TESTING AND EVALUATION BP 235 B-45 EP 237 PG 3 JI J. Test. Eval. PY 1994 PD MAY VL 22 IS 3 GA NJ542 J9 J TEST EVAL UT ISI:A1994NJ54200009 PT J AU POLSKI, PA TI INTERNATIONAL AVIATION SECURITY RESEARCH-AND-DEVELOPMENT SO JOURNAL OF TESTING AND EVALUATION BP 267 EP 274 PG 8 JI J. Test. Eval. PY 1994 PD MAY VL 22 IS 3 GA NJ542 J9 J TEST EVAL UT ISI:A1994NJ54200019 PT J AU ZELLWEGER, AG TI SIMULATIONS TCAS ROLE DETAILED SO AVIATION WEEK & SPACE TECHNOLOGY BP 8 EP 8 PG 1 JI Aviat. Week Space Technol. PY 1994 PD JAN 24 VL 140 IS 4 GA NF332 J9 AVIAT WEEK SPACE TECHNOL UT ISI:A1994NF33200001
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: JI Aerosp. Am. PY 1996 PD JUN VL 34
Page 47 and 48: VL 62 IS 3 GA EZ171 J9 AVIAT SPACE
Page 49 and 50: AU MASON, RE HSIAO, TT TI WORKFORCE
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
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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
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NR 58 CR *N ATL TREAT ORG, 1972, AG
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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
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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
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avoidance data using on-board measu
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helicopters. Subsequent flight test
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improvement had to come from the on
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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
Page 159 and 160:
stabilization, Synthetic Vision for
Page 161 and 162:
wing aircraft where weight is of pa
Page 163 and 164:
The reduction of the minimum altitu
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provided substantial improvements i
Page 167 and 168:
Honeywell has conducted a series of
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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,
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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
Page 201 and 202:
systems is the weight savings resul
Page 203 and 204:
of two rows of three-abreast seatin
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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
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Conference Proceeding, 52, McCauley
Page 215 and 216:
mode shapes, which are suitable for
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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
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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
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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
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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,
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ased upon a relatively straightforw
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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
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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
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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
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CY - New York, NY, USA PB - IEEE AD
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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
Page 317 and 318:
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
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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-
Page 347 and 348:
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-
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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
Page 423 and 424:
PY- cJan 95 PG- 10p NT- In AGARD, L
Page 425 and 426:
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
Page 431 and 432:
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
Page 437 and 438:
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
Page 471 and 472:
AU- McAnulty, D. M. ; Ruffner, J. W
Page 473 and 474:
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
Page 503 and 504:
de Vision Nocturne) Held in Pensaco
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Operations. The tests were conducte
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Lateral range curves and sweep widt
Page 509 and 510:
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
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; Vision; Comfort; Flight clothing;
Page 523 and 524:
helmet-mounted display. The experim
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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
Page 537 and 538:
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
Page 569 and 570:
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
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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;
Page 623 and 624:
Road, Springfield, VA, 22161, USA.
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AB- Thirteen subanalyses were perfo
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Directly related functions included
Page 629 and 630:
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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Page 677 and 678:
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
Page 685 and 686:
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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Page 727 and 728:
CS- Army Aeromedical Research Lab.,
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PG- 48p NT- See also Volume 9, AD-A
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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
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PY- 24 Mar 80 PG- 16p NT- Trans. of
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PY- Feb 80 PG- 55p NT- Order this p
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presents the facts, conditions, cir
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AU- Robertson, D. G. CS- Department
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AZ- 0792294 AA- N79-32834/0/XAB TI
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attention inside the cockpit. (Auth
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Flight crews; Fatigue; Human factor
Page 759 and 760:
discussions. The data collected ind
Page 761 and 762:
(Communication--Verbal) AZ- 0734790
Page 763 and 764:
accuracy of theoretical flow field
Page 765 and 766:
RN- USAARL-SPECIAL BIB-SER-9-SUP-1
Page 767 and 768:
AB- The results of test programs co
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Charge/Detonation System; Dice Thro
Page 771 and 772:
sensors, a cooling generator, and a
Page 773 and 774:
at (703)321-8547; and email at orde
Page 775 and 776:
Page 777 and 778:
information content was entirely de
Page 779 and 780:
CN- NONR414800 PY- Feb 65 PG- 64p N
Page 781 and 782:
toxicology evaluation are continuin
Page 783 and 784:
Page 785 and 786:
NT- Distribution limitation now rem
Page 787 and 788:
is more effective than either of th
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PC- PC A06/MF A01 JA- GRAI7710 AB-
Page 791 and 792:
countries); fax at (703)321-8547; a
Page 793 and 794:
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
Page 801 and 802:
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
Page 807 and 808:
SH- 51B (Aeronautics and Aerodynami
Page 809 and 810:
AZ- 0577573 AA- AD-871 350/5/XAB T
Page 811 and 812:
NT- Distribution limitation now rem
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PY- Nov 70 PG- 190p NT- Distributio
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Page 817 and 818:
Page 819 and 820:
(Ordnance--Guns) AZ- 0570727 AA- A
Page 821 and 822:
AZ- 0569991 AA- AD-923 214/1/XAB T
Page 823 and 824:
AB- The expanded service test of th
Page 825 and 826:
Calibration ID- *Uh-1n aircraft; Ca
Page 827 and 828:
CS- 332500 CN- DAHC19-71-C-0021; S
Page 829 and 830:
AZ- 0567498 AA- AD-881 186/1/XAB T
Page 831 and 832:
SH- 68B (Environmental Pollution an
Page 833 and 834:
Page 835 and 836:
controlling the airspeed of a helic
Page 837 and 838:
Considerations TI- Final rept. 30
Page 839 and 840:
from flight test data. The programs
Page 841 and 842:
supplies, and sample transcripts of
Page 843 and 844:
DE- *Microphones; *Noise reduction;
Page 845 and 846:
Page 847 and 848:
CS- Army Materiel Command Texarkana
Page 849 and 850:
assigning the crews for the field t
Page 851 and 852:
tracking, parachutes, balloon telem
Page 853 and 854:
oute structure in the New York area
Page 855 and 856:
SH- 74E (Military Sciences--Logisti
Page 857 and 858:
during April and June 1973. (Author
Page 859 and 860:
AZ- 0456286 AA- N74-27504/1/XAB TI
Page 861 and 862:
the criteria values. (Author) DE- *
Page 863 and 864:
claims. Most all the projects on wa
Page 865 and 866:
PC- PC A07/MF A01 JA- GRAI7408 AB-
Page 867 and 868:
AB- The report describes POBAL, a t
Page 869 and 870:
JA- GRAI7319 AB- A higher harmonic
Page 871 and 872:
AB- Three experiments designed to d
Page 873 and 874:
AA- AD-751 217/XAB TI- High Perfor
Page 875 and 876:
SH- 92B (Behavior and Society--Psyc
Page 877 and 878:
DE- *Pilots; *Visual perception; *H
Page 879 and 880:
AZ- 0297921 AA- AD-733 671/XAB TI-
Page 881 and 882:
of VTOL aircraft and helicopters. A
Page 883 and 884:
Development--Emergency Services and
Page 885 and 886:
ID- C-142 aircraft; Gust alleviatio
Page 887 and 888:
Page 889 and 890:
conducted at Edwards Air Force Base
Page 891 and 892:
PY- 1969 PG- 135p NT- Proceedings o
Page 893 and 894:
Page 895 and 896:
helicopter and second the effect th
Page 897 and 898:
AZ- 0190814 AA- AD-691 299/XAB TI-
Page 899 and 900:
AZ- 0182500 AA- N69-21707/XAB TI-
Page 901 and 902:
CS- 142925 RN- TR-1-214-VOL-1; HS-
Page 903 and 904:
PY- Feb 68 PG- 30p NT- Order this p
Page 905 and 906:
multivariable vehicular control sys
Page 907 and 908:
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:
Page 917 and 918:
situation. (Author) DE- *Aviation p
Page 919 and 920:
RN- JANAIR-TR-D228-100-011 CN- NONR
Page 921 and 922:
een completed. From the information
Page 923 and 924:
TI- State of the ART for V/STOL Con
Page 925 and 926:
fixed-wind flyable system and two r
Page 927 and 928:
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
Page 933 and 934:
including NVG and HMD are offered w
Page 935 and 936:
AN- 02559555 AN- A01-17563 TI- Fi
Page 937 and 938:
SH- 7554 Man/System Technology & Li
Page 939 and 940:
TI- Evaluation of algorithms for fu
Page 941 and 942:
AN- 02535822 AN- A00-46831 TI- Ca
Page 943 and 944:
TI- Evaluation of a motion fidelity
Page 945 and 946:
REFUELING; PERSONAL COMPUTERS; ALGO
Page 947 and 948:
PD- 199900 RF- 18 LA- English GL- G
Page 949 and 950:
technology is currently available t
Page 951 and 952:
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
Page 963 and 964:
GL- United States CP- United States
Page 965 and 966:
AN- A99-40429 TI- Helmet-mounted d
Page 967 and 968:
were analyzed using frequency domai
Page 969 and 970:
missions. The development, integrat
Page 971 and 972:
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
Page 977 and 978:
RN- NASA no. 19990025678 LA- Englis
Page 979 and 980:
RN- NASA no. 19980218991 LA- Englis
Page 981 and 982:
communication system. Sixteen air t
Page 983 and 984:
A stepwise multiple regression foun
Page 985 and 986:
partial restoration of recordings b
Page 987 and 988:
DE- HUMAN FACTORS ENGINEERING; IN-F
Page 989 and 990:
own recollections and involvement i
Page 991 and 992:
displays in lieu of miniaturized CR
Page 993 and 994:
SH- 7581 Administration & Managemen
Page 995 and 996:
AN- 02347126 AN- A98-27588 TI- An
Page 997 and 998:
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
Page 1007 and 1008:
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
Page 1013 and 1014:
Page 1015 and 1016:
DE- HARDWARE; PERFORMANCE TESTS; FL
Page 1017 and 1018:
Page 1019 and 1020:
weaknesses relative to the harness
Page 1021 and 1022:
AN- 02292483 AN- N97-10549 TI- Vi
Page 1023 and 1024:
AV- CASI HC A03/MF A04 JA- STAR961
Page 1025 and 1026:
manufacturers, research institution
Page 1027 and 1028:
SH- 7503 Air Transportation & Safet
Page 1029 and 1030:
AB- There is a need for calibrated
Page 1031 and 1032:
helicopters of different weight (li
Page 1033 and 1034:
JA- IAA9612 AB- Indonesian Air Forc
Page 1035 and 1036:
AN- 02259646 AN- A96-44927 TI- De
Page 1037 and 1038:
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-
Page 1057 and 1058:
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
Page 1083 and 1084:
DT- CONFERENCE PAPER AV- AIAA Tech
Page 1085 and 1086:
involved a delay of rise times afte
Page 1087 and 1088:
DE- *AIRCRAFT PILOTS; *HELICOPTERS
Page 1089 and 1090:
intermittently. Instructions in Exp
Page 1091 and 1092:
SO- In: AHS, Annual Forum, 49th, Sa
Page 1093 and 1094:
AN- 02128051 AN- A94-19165 TI- Ev
Page 1095 and 1096:
PD- 199300 RF- 6 LA- English GL- Un
Page 1097 and 1098:
TI- Flight tests of the digitally c
Page 1099 and 1100:
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
Page 1107 and 1108:
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
Page 1113 and 1114:
AB- Tests conducted on a variety of
Page 1115 and 1116:
SH- 7506 Aircraft Instrumentation (
Page 1117 and 1118:
AU- VOLODKO, A. M.; VERKHOZIN, M. P
Page 1119 and 1120:
professional'nuiu nadezhnost' letch
Page 1121 and 1122:
ecent sea trials are examined. (Aut
Page 1123 and 1124:
Page 1125 and 1126:
AN- 02032965 AN- N92-17165 TI- Sy
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AN- 02027444 AN- N92-11629 TI- Pe
Page 1129 and 1130:
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
Page 1139 and 1140:
AN- 01984386 AN- A92-16050 TI- Fl
Page 1141 and 1142:
and convenient means of acquiring t
Page 1143 and 1144:
Page 1145 and 1146:
DE- *ANTHROPOMETRY; *HELICOPTER PE
Page 1147 and 1148:
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
Page 1159 and 1160:
SN- 0360-5450 LA- English GL- Germa
Page 1161 and 1162:
TESTS; FRACTURE MECHANICS; HUMAN FA
Page 1163 and 1164:
DE- *AH-64 HELICOPTER; *AVIONICS;
Page 1165 and 1166:
RN- AIAA PAPER 90-3172 LA- English
Page 1167 and 1168:
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
Page 1173 and 1174:
SN- 0091-3286 LA- English GL- Unite
Page 1175 and 1176:
AN- 01877767 AN- A90-42495 TI- He
Page 1177 and 1178:
HELICOPTER TAIL ROTORS; HIGH STRENG
Page 1179 and 1180:
attention. The different assumption
Page 1181 and 1182:
SH- 7506 Aircraft Instrumentation (
Page 1183 and 1184:
DE- *CONTROL SYSTEMS DESIGN; *FLIG
Page 1185 and 1186:
AN- 01863439 AN- A90-28167 TI- HA
Page 1187 and 1188:
CP- United States DT- CONFERENCE PA
Page 1189 and 1190:
AN- 01854825 AN- A90-19553 TI- Si
Page 1191 and 1192:
approach, a control aid program ope
Page 1193 and 1194:
Page 1195 and 1196:
SO- IN: AIAA Flight Simulation Tech
Page 1197 and 1198:
of modern military helicopters are
Page 1199 and 1200:
analyzed for content, agencies invo
Page 1201 and 1202:
DT- PREPRINT AV- AIAA Technical Li
Page 1203 and 1204:
tilt-rotor aircraft, as derived fro
Page 1205 and 1206:
ecently implemented OH-6A helicopte
Page 1207 and 1208:
Page 1209 and 1210:
AU- FITZPATRICK, DANIEL T. (Hawaii,
Page 1211 and 1212:
DT- REPORT AV- AIAA Technical Libr
Page 1213 and 1214:
AB- The National Transportation Saf
Page 1215 and 1216:
AN- A88-53659 TI- Determination of
Page 1217 and 1218:
*NAVIGATION INSTRUMENTS; *VIDEO EQU
Page 1219 and 1220:
PD- 198700 RF- 23 LA- English GL- U
Page 1221 and 1222:
JA- IAA8817 AB- One- and two-person
Page 1223 and 1224:
Page 1225 and 1226:
development of turbines, ramjet eng
Page 1227 and 1228:
(STAR) aircraft. The STAR, a one-of
Page 1229 and 1230:
AU- PELEGRIN, MARC J. (ONERA, Centr
Page 1231 and 1232:
DE- ATTITUDE CONTROL; CONTROL SIMUL
Page 1233 and 1234:
NT- Colloquium held in Brunswick, W
Page 1235 and 1236:
Page 1237 and 1238:
AB- The prevalence of backache amon
Page 1239 and 1240:
AB- Helicopter pilots were used to
Page 1241 and 1242:
sizes and distances in the visual s
Page 1243 and 1244:
*FLIGHT TESTS; *MANUAL CONTROL; *ME
Page 1245 and 1246:
SF- DTIC DE- *ANTIEMETICS AND ANTI
Page 1247 and 1248:
DE- *CONFERENCES; *FLIGHT SIMULATI
Page 1249 and 1250:
GL- United Kingdom CP- Germany DT-
Page 1251 and 1252:
Page 1253 and 1254:
SH- 7505 Aircraft Design, Testing &
Page 1255 and 1256:
Page 1257 and 1258:
JA- IAA8713 AB- A topographic map a
Page 1259 and 1260:
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
Page 1265 and 1266:
PD- 198500 RF- 287 LA- Russian GL-
Page 1267 and 1268:
DE- CONTROL STABILITY; FEEDBACK CON
Page 1269 and 1270:
GL- Germany CP- Germany DT- CONFERE
Page 1271 and 1272:
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
Page 1277 and 1278:
Black Hawk. The program phases incl
Page 1279 and 1280:
LA- English GL- Australia CP- Unite
Page 1281 and 1282:
AN- 01602456 AN- A86-26004 TI- AI
Page 1283 and 1284:
AN- 01600170 AN- A86-23718 TI- Re
Page 1285 and 1286:
flight, and a requirement for the p
Page 1287 and 1288:
Page 1289 and 1290:
AN- 01590810 AN- A86-14356 TI- Th
Page 1291 and 1292:
GL- Germany CP- International Organ
Page 1293 and 1294:
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
Page 1301 and 1302:
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
Page 1379 and 1380:
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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