FLYING QUALITIES OF PILOTED AIRCRAFT - CAFE Foundation

More documents

Recommendations

Info

MIL–STD–1797AAPPENDIX A2ζ d ω d 2ζ ζ ω φ φCiρgV 2(W/S)ρgV2(W/S)Cy βCnr22k z y C 1β 2k 2 zk z 2k x2CnrC βCC nβ L1C δ a CCr δ aC n p22k z C i Cn i xz z1 – xz 2 C Cn Cii xz xni2 /( xz)1 – xz/( xz) yδ a CCβδ aC L 1 W/(qS),k x22 /(mb ).xk 2 2z = /(mb ).zand control derivatives include the effects of any crossfeeds.VERIFICATION LESSONS LEARNED418
MIL–STD–1797AAPPENDIX A4.5.1.5 Roll time delay. The value of the equivalent time delay, ep, shall be no greater than ____________.REQUIREMENT RATIONALE (4.5.1.5)This requirement is intended to insure that the combined delay contributions of prefilters, stabilityaugmentation, servos, etc., does not degrade the pilot’s tracking capability in roll control.REQUIREMENT GUIDANCEThe related MIL–F–8785C requirement is paragraph 3.5.3.Recommended values of τep, which is defined in 4.5.1.1, are given in table XXVII.TABLE XXVII. Recommended allowable equivalent delay.LEVELALLOWABLE DELAY(sec)1 0.102 0.203 0.25Based upon extensive research into the effect of time delays in the pitch axis, the important contribution ofdelays is well known. This requirement extends to the roll axis the τe limits imposed on the pitch axis in4.2.1.2. For lack of enough substantive data, the limits remain unchanged from MIL–F–8785C. Precise rolltracking, like pitch tracking, is a high–bandwidth task. As more data become available, these limits should beevaluated and adjusted if necessary.4.5.1.1, which sets roll mode limits, discusses the use of equivalent system matching of the roll rate responseto roll controller to extract TS, TR, and ep. That section should be consulted for more information on themeaning of τep.SUPPORTING DATALittle in the way of hard data is available. However, the effect of equivalent time delay was found to besignificant in the longitudinal axis (see 4.2.1.1).This result is seen to extend to the lateral axis based upon theLATHOS study of AFWAL–TR–81–3171 (figure 168). In fact, for the demanding task used in the LATHOSprogram (air–to–air refueling and bank angle tracking on the HUD), any time delay above the basic NT–33value resulted in Level 2 ratings. AFWAL–TR–81–3118 reports similarly that for simulated large transports inapproach and landing any increase above the basic (0.12 sec) effective time delay could not support Level 1ratings (figure 169). Hence there is at least evidence to support a need for such a requirement, thougheffective time delay may be more critical in the lateral than in the longitudinal axis.REQUIREMENT LESSONS LEARNED419
Page 1 and 2:
NOTE: MIL-STD-1797A has been redesi
Page 3 and 4:
MIL-STD-1797AFOREWORDThis standard
Page 5 and 6:
MIL-STD-1797ACONTENTS - ContinuedPa
Page 7 and 8:
Page 9 and 10:
Page 11 and 12:
Page 13 and 14:
Page 15 and 16:
MIL-STD-1797A1. SCOPE1.1 Purpose. T
Page 17 and 18:
MIL-STD-1797AT 2 Time to double amp
Page 19 and 20:
MIL-STD-1797AV end Speed for maximu
Page 21 and 22:
MIL-STD-1797Aω spUndamped natural
Page 23 and 24:
MIL-STD-1797Awhere p , p and p are
Page 25 and 26:
MIL-STD-1797AFIGURE 1. Roll-sidesli
Page 27 and 28:
MIL-STD-1797AFIGURE 2. Roll-sidesli
Page 29 and 30:
MIL-STD-1797AExamples showing measu
Page 31 and 32:
MIL-STD-1797Aσ, RMS Root-mean-squa
Page 33 and 34:
MIL-STD-1797A4. REQUIREMENTS4.1 Gen
Page 35 and 36:
MIL-STD-1797Athe selected configura
Page 37 and 38:
MIL-STD-1797Ab. For these calculati
Page 39 and 40:
MIL-STD-1797Aindicate to the pilot
Page 41 and 42:
MIL-STD-1797Aaccessibly located, co
Page 43 and 44:
MIL-STD-1797ATABLE IV. Pitch trim c
Page 45 and 46:
MIL-STD-1797Aspeed range by the mos
Page 47 and 48:
MIL-STD-1797Ato designated flight p
Page 49 and 50:
MIL-STD-1797Ainputs are simple, eas
Page 51 and 52:
MIL-STD-1797ARight yaw-control-peda
Page 53 and 54:
MIL-STD-1797Ad. Yaw axis control po
Page 55 and 56:
MIL-STD-1797ADuring combat-type man
Page 57 and 58:
MIL-STD-1797A4.9 Flying qualities r
Page 59 and 60:
MIL-STD-1797A5. VERIFICATION5.1 Gen
Page 61 and 62:
MIL-STD-1797A5.1.12.4 Rate of contr
Page 63 and 64:
MIL-STD-1797A5.2.8.6.5 Pitch axis c
Page 65 and 66:
MIL-STD-1797A5.5.9.3 Roll axis cont
Page 67 and 68:
MIL-STD-1797A5.8 Flying qualities r
Page 69 and 70:
MIL-STD-1797A1st Tier References2nd
Page 71 and 72:
MIL-STD-1797AAPPENDIX AFLYING QUALI
Page 73 and 74:
MIL-STD-1797AAPPENDIX AASD-TDR-63-3
Page 75 and 76:
MIL-STD-1797AAPPENDIX AAFFDL-TR-70-
Page 77 and 78:
MIL-STD-1797AAPPENDIX AAFWAL-TR-81-
Page 79 and 80:
MIL-STD-1797AAPPENDIX AFAA-RD-70-65
Page 81 and 82:
MIL-STD-1797AAPPENDIX ANASA-TM-X-62
Page 83 and 84:
MIL-STD-1797AAPPENDIX AAIAA Paper 6
Page 85 and 86:
MIL-STD-1797AAPPENDIX ABoeing D6-10
Page 87 and 88:
MIL-STD-1797AAPPENDIX AAGARD-CP-333
Page 89 and 90:
MIL-STD-1797AAPPENDIX ANeal, T. Pet
Page 91 and 92:
MIL-STD-1797AAPPENDIX AFor military
Page 93 and 94:
MIL-STD-1797AAPPENDIX AFIGURE 3. Cl
Page 95 and 96:
MIL-STD-1797AAPPENDIX Ab. Cruise (C
Page 97 and 98:
MIL-STD-1797AAPPENDIX AWhile the or
Page 99 and 100:
MIL-STD-1797AAPPENDIX A3.3 Levels a
Page 101 and 102:
MIL-STD-1797AAPPENDIX AFractional r
Page 103 and 104:
MIL-STD-1797AAPPENDIX A40. REQUIREM
Page 105 and 106:
MIL-STD-1797AAPPENDIX AREQUIREMENT
Page 107 and 108:
MIL-STD-1797AAPPENDIX AVERIFICATION
Page 109 and 110:
MIL-STD-1797AAPPENDIX ASome Flight
Page 111 and 112:
MIL-STD-1797AAPPENDIX ATABLE I. Ope
Page 113 and 114:
MIL-STD-1797AAPPENDIX AIf design tr
Page 115 and 116:
MIL-STD-1797AAPPENDIX Ac. The speed
Page 117 and 118:
MIL-STD-1797AAPPENDIX A4.1.4.3 Perm
Page 119 and 120:
MIL-STD-1797AAPPENDIX A4.1.5 Config
Page 121 and 122:
MIL-STD-1797AAPPENDIX A4.1.6 Aircra
Page 123 and 124:
Page 125 and 126:
MIL-STD-1797AAPPENDIX A4.1.7.1 Allo
Page 127 and 128:
MIL-STD-1797AAPPENDIX Aart can supp
Page 129 and 130:
MIL-STD-1797AAPPENDIX ATABLE VIII.
Page 131 and 132:
MIL-STD-1797AAPPENDIX AP(Level 2) =
Page 133 and 134:
MIL-STD-1797AAPPENDIX ASee also REQ
Page 135 and 136:
MIL-STD-1797AAPPENDIX Ademonstrated
Page 137 and 138:
MIL-STD-1797AAPPENDIX A4.1.7.4 Gene
Page 139 and 140:
MIL-STD-1797AAPPENDIX A5.1.7.4 Gene
Page 141 and 142:
MIL-STD-1797AAPPENDIX A4.1.7.6 Fail
Page 143 and 144:
Page 145 and 146:
MIL-STD-1797AAPPENDIX A4.1.10 Inter
Page 147 and 148:
Page 149 and 150:
Page 151 and 152:
MIL-STD-1797AAPPENDIX A4.1.11.2 Rel
Page 153 and 154:
MIL-STD-1797AAPPENDIX A4.1.11.4 Fai
Page 155 and 156:
MIL-STD-1797AAPPENDIX ATABLE IX. Su
Page 157 and 158:
MIL-STD-1797AAPPENDIX A4.1.11.5 Con
Page 159 and 160:
MIL-STD-1797AAPPENDIX Aone must con
Page 161 and 162:
MIL-STD-1797AAPPENDIX AUnless deact
Page 163 and 164:
MIL-STD-1797AAPPENDIX ATABLE X. Con
Page 165 and 166:
MIL-STD-1797AAPPENDIX A4.1.11.6 Pil
Page 167 and 168:
MIL-STD-1797AAPPENDIX A4.1.11.7 Res
Page 169 and 170:
Page 171 and 172:
While some functions that might be
Page 173 and 174:
MIL-STD-1797AAPPENDIX A4.1.12.4 Rat
Page 175 and 176:
LevelMIL-STD-1797AAPPENDIX ATABLE X
Page 177 and 178:
MIL-STD-1797AAPPENDIX Athunderstorm
Page 179 and 180:
MIL-STD-1797AAPPENDIX AThe irrevers
Page 181 and 182:
MIL-STD-1797AAPPENDIX A4.2 Flying q
Page 183 and 184:
MIL-STD-1797AAPPENDIX Achanges sign
Page 185 and 186:
MIL-STD-1797AAPPENDIX A4.2.1.2 Shor
Page 187 and 188:
MIL-STD-1797AAPPENDIX Apilot pitch
Page 189 and 190:
THE EQUIVALENT SYSTEMS CONCEPTMIL-S
Page 191 and 192:
MIL-STD-1797AAPPENDIX AIt is assume
Page 193 and 194:
MIL-STD-1797AAPPENDIX AThe problem
Page 195 and 196:
MIL-STD-1797AAPPENDIX AFIGURE 15. E
Page 197 and 198:
MIL-STD-1797AAPPENDIX AFIGURE 16. C
Page 199 and 200:
MIL-STD-1797AAPPENDIX AFIGURE 19. P
Page 201 and 202:
MIL-STD-1797AAPPENDIX AFor many air
Page 203 and 204:
MIL-STD-1797AAPPENDIX AFIGURE 22. T
Page 205 and 206:
MIL-STD-1797AAPPENDIX AFIGURE 24. R
Page 207 and 208:
MIL-STD-1797AAPPENDIX AThe last fac
Page 209 and 210:
MIL-STD-1797AAPPENDIX AShort-period
Page 211 and 212:
Page 213 and 214:
Page 215 and 216:
MIL-STD-1797AAPPENDIX AFIGURE 36. A
Page 217 and 218:
MIL-STD-1797AAPPENDIX Aimposed on l
Page 219 and 220:
Page 221 and 222:
Page 223 and 224:
Page 225 and 226:
MIL-STD-1797AAPPENDIX ALAHOS data (
Page 227 and 228:
Page 229 and 230:
Page 231 and 232:
C. Transient peak ratio, rise time,
Page 233 and 234:
MIL-STD-1797AAPPENDIX Acriteria do
Page 235 and 236:
Page 237 and 238:
MIL-STD-1797AAPPENDIX AThe AFFDL-TR
Page 239 and 240:
MIL-STD-1797AAPPENDIX AD. Bandwidth
Page 241 and 242:
MIL-STD-1797AAPPENDIX AFIGURE 58. S
Page 243 and 244:
MIL-STD-1797AAPPENDIX AFIGURE 59. D
Page 245 and 246:
Page 247 and 248:
Page 249 and 250:
Page 251 and 252:
MIL-STD-1797AAPPENDIX AE. Closed-Lo
Page 253 and 254:
MIL-STD-1797AAPPENDIX AThe criteria
Page 255 and 256:
Page 257 and 258:
MIL-STD-1797AAPPENDIX AConfiguratio
Page 259 and 260:
Page 261 and 262:
MIL-STD-1797AAPPENDIX AFIGURE 76. H
Page 263 and 264:
Page 265 and 266:
MIL-STD-1797AAPPENDIX A* Pitch rate
Page 267 and 268:
MIL-STD-1797AAPPENDIX APHASE LAGFor
Page 269 and 270:
MIL-STD-1797AAPPENDIX Ahorizontal t
Page 271 and 272:
Page 273 and 274:
MIL-STD-1797AAPPENDIX Aa. AnalysisA
Page 275 and 276:
MIL-STD-1797AAPPENDIX ACare must be
Page 277 and 278:
MIL-STD-1797AAPPENDIX AFIGURE 89a.
Page 279 and 280:
Page 281 and 282:
MIL-STD-1797AAPPENDIX A4.2.2 Pilot-
Page 283 and 284:
MIL-STD-1797AAPPENDIX Afeature at t
Page 285 and 286:
MIL-STD-1797AAPPENDIX AThe correspo
Page 287 and 288:
MIL-STD-1797AAPPENDIX AωBWτ p= 1.
Page 289 and 290:
MIL-STD-1797AAPPENDIX A275
Page 291 and 292:
Page 293 and 294:
Page 295 and 296:
MIL-STD-1797AAPPENDIX A4.2.5 Pitch
Page 297 and 298:
4.2.6. Pitch axis response to other
Page 299 and 300:
MIL-STD-1797AAPPENDIX A4.2.6.2 Pitc
Page 301 and 302:
Page 303 and 304:
Page 305 and 306:
MIL-STD-1797AAPPENDIX A5.2.7.2.1 Lo
Page 307 and 308:
MIL-STD-1797AAPPENDIX AFIGURE 96. N
Page 309 and 310:
Page 311 and 312:
Page 313 and 314:
Page 315 and 316:
MIL-STD-1797AAPPENDIX AIt must be s
Page 317 and 318:
MIL-STD-1797AAPPENDIX ATABLE XVII.
Page 319 and 320:
MIL-STD-1797AAPPENDIX AFIGURE 100.
Page 321 and 322:
MIL-STD-1797AAPPENDIX Aratings show
Page 323 and 324:
Page 325 and 326:
Page 327 and 328:
MIL-STD-1797AAPPENDIX AAccording to
Page 329 and 330:
MIL-STD-1797AAPPENDIX A[The Citabri
Page 331 and 332:
MIL-STD-1797AAPPENDIX AFor a revers
Page 333 and 334:
MIL-STD-1797AAPPENDIX Arequirements
Page 335 and 336:
Page 337 and 338:
Page 339 and 340:
MIL-STD-1797AAPPENDIX ASome additio
Page 341 and 342:
Page 343 and 344:
MIL-STD-1797AAPPENDIX ATABLE XVIII.
Page 345 and 346:
Page 347 and 348:
Page 349 and 350:
MIL-STD-1797AAPPENDIX AGiven some v
Page 351 and 352:
Page 353 and 354:
MIL-STD-1797AAPPENDIX A4.2.8.6.2 Pi
Page 355 and 356:
Page 357 and 358:
Page 359 and 360:
Page 361 and 362:
Page 363 and 364:
Page 365 and 366:
Page 367 and 368:
4.3.1 Flight path response to attit
Page 369 and 370:
MIL-STD-1797AAPPENDIX ATABLE XXIII.
Page 371 and 372:
MIL-STD-1797AAPPENDIX A4.3.1.2 Stea
Page 373 and 374:
MIL-STD-1797AAPPENDIX Adγdδe γ
Page 375 and 376:
Page 377 and 378:
MIL-STD-1797AAPPENDIX ACombinations
Page 379 and 380:
Page 381 and 382: MIL-STD-1797AAPPENDIX A4.3.2 Flight
Page 383 and 384: MIL-STD-1797AAPPENDIX AVERIFICATION
Page 385 and 386: MIL-STD-1797AAPPENDIX AFor all but
Page 387 and 388: MIL-STD-1797AAPPENDIX AThe accelera
Page 389 and 390: MIL-STD-1797AAPPENDIX A4.4.1.1 Spee
Page 391 and 392: 4.5 Flying qualities requirements f
Page 393 and 394: MIL-STD-1797AAPPENDIX APrinceton Un
Page 395 and 396: MIL-STD-1797AAPPENDIX AFIGURE 135.
Page 401 and 402: MIL-STD-1797AAPPENDIX AExamination
Page 403 and 404: MIL-STD-1797AAPPENDIX AReduction of
Page 405 and 406: MIL-STD-1797AAPPENDIX AC L 1___ 1-
Page 407 and 408: MIL-STD-1797AAPPENDIX ACRUISE CONDI
Page 409 and 410: MIL-STD-1797AAPPENDIX ABearing in m
Page 411 and 412: MIL-STD-1797AAPPENDIX Alanding appr
Page 415 and 416: MIL-STD-1797AAPPENDIX AHowever, NAS
Page 417 and 418: MIL-STD-1797AAPPENDIX A2 ζ ωRS RS
Page 421 and 422: MIL-STD-1797AAPPENDIX Aallowed to b
Page 425 and 426: MIL-STD-1797AAPPENDIX ASUPPORTING D
Page 429 and 430: MIL-STD-1797AAPPENDIX Aa) Positive
Page 431: MIL-STD-1797AAPPENDIX A5.5.1.4 Roll
Page 435 and 436: MIL-STD-1797AAPPENDIX A5.5.1.5 Time
Page 437 and 438: MIL-STD-1797AAPPENDIX A4.5.3 Linear
Page 439 and 440: MIL-STD-1797AAPPENDIX ANOTES:1. Fla
Page 441 and 442: MIL-STD-1797AAPPENDIX Aand in a ste
Page 443 and 444: MIL-STD-1797AAPPENDIX A5.5.5 Roll c
Page 445 and 446: 4.5.7 Roll axis response to other i
Page 447 and 448: MIL-STD-1797AAPPENDIX A4.5.7.2 Roll
Page 449 and 450: MIL-STD-1797AAPPENDIX ATABLE XXVIII
Page 451 and 452: MIL-STD-1797AAPPENDIX ATABLE XXX. R
Page 453 and 454: MIL-STD-1797AAPPENDIX ADiscussion o
Page 457 and 458: MIL-STD-1797AAPPENDIX AAψ= V o β+
Page 459 and 460: MIL-STD-1797AAPPENDIX Aroll respons
Page 461 and 462: MIL-STD-1797AAPPENDIX AClass IV air
Page 463 and 464: MIL-STD-1797AAPPENDIX A-155-155FIGU
Page 467 and 468: MIL-STD-1797AAPPENDIX Anondivergent
Page 475 and 476: MIL-STD-1797AAPPENDIX AwhereC nδ
Page 477 and 478: MIL-STD-1797AAPPENDIX A4.5.8.3 Roll
Page 479 and 480: MIL-STD-1797AAPPENDIX AThe third sk
Page 481 and 482: MIL-STD-1797AAPPENDIX AVERIFICATION
Page 483 and 484:
MIL-STD-1797AAPPENDIX A4.5.8.6 Roll
Page 485 and 486:
Page 487 and 488:
Page 489 and 490:
Page 491 and 492:
Page 493 and 494:
Page 495 and 496:
Page 497 and 498:
Page 499 and 500:
Page 501 and 502:
Page 503 and 504:
Page 505 and 506:
MIL-STD-1797AAPPENDIX AThe LATHOS r
Page 507 and 508:
MIL-STD-1797AAPPENDIX Apound). It c
Page 509 and 510:
Page 511 and 512:
Page 513 and 514:
MIL-STD-1797AAPPENDIX A4.5.9.5.2 Ro
Page 515 and 516:
Page 517 and 518:
Page 519 and 520:
Page 521 and 522:
MIL-STD-1797AAPPENDIX AIt should al
Page 523 and 524:
Page 525 and 526:
Page 527 and 528:
Page 529 and 530:
Page 531 and 532:
MIL-STD-1797AAPPENDIX AIn the fligh
Page 533 and 534:
Page 535 and 536:
Page 537 and 538:
MIL-STD-1797AAPPENDIX AIt has long
Page 539 and 540:
MIL-STD-1797AAPPENDIX AAn evaluatio
Page 541 and 542:
Page 543 and 544:
Page 545 and 546:
MIL-STD-1797AAPPENDIX A4.6.1.3 Wing
Page 547 and 548:
MIL-STD-1797AAPPENDIX AThe bandwidt
Page 549 and 550:
Page 551 and 552:
MIL-STD-1797AAPPENDIX AConfiguratio
Page 553 and 554:
MIL-STD-1797AAPPENDIX Arestraint wi
Page 555 and 556:
MIL-STD-1797AAPPENDIX ATABLE XLIII.
Page 557 and 558:
Page 559 and 560:
MIL-STD-1797AAPPENDIX ASUPPORTING D
Page 561 and 562:
Page 563 and 564:
MIL-STD-1797AAPPENDIX AP-3B (Class
Page 565 and 566:
Page 567 and 568:
Page 569 and 570:
MIL-STD-1797AAPPENDIX AThe ability
Page 571 and 572:
MIL-STD-1797AAPPENDIX AFor augmente
Page 573 and 574:
Page 575 and 576:
MIL-STD-1797AAPPENDIX AHowever, bef
Page 577 and 578:
C. r o/po Near ZeroMIL-STD-1797AAPP
Page 579 and 580:
MIL-STD-1797AAPPENDIX AD. Complex R
Page 581 and 582:
Page 583 and 584:
MIL-STD-1797AAPPENDIX A7. If 0.03 <
Page 585 and 586:
MIL-STD-1797AAPPENDIX A4.6.4 Yaw ax
Page 587 and 588:
MIL-STD-1797AAPPENDIX Aand the time
Page 589 and 590:
Page 591 and 592:
MIL-STD-1797AAPPENDIX AβC nδa C C
Page 593 and 594:
MIL-STD-1797AAPPENDIX A4.6.5.2. Yaw
Page 595 and 596:
MIL-STD-1797AAPPENDIX A4.6.6 Yaw ax
Page 597 and 598:
Page 599 and 600:
MIL-STD-1797AAPPENDIX A4.6.6.3 Yaw
Page 601 and 602:
Page 603 and 604:
MIL-STD-1797AAPPENDIX AC yβCβ0δa
Page 605 and 606:
Page 607 and 608:
Page 609 and 610:
Page 611 and 612:
Page 613 and 614:
Page 615 and 616:
MIL-STD-1797AAPPENDIX Ato augment Y
Page 617 and 618:
MIL-STD-1797AAPPENDIX AUse of such
Page 619 and 620:
in terms of the uncoupled approxima
Page 621 and 622:
Page 623 and 624:
Page 625 and 626:
MIL-STD-1797AAPPENDIX AMultiaxis, n
Page 627 and 628:
MIL-STD-1797AAPPENDIX ATABLE LI. Di
Page 629 and 630:
MIL-STD-1797AAPPENDIX AA critical d
Page 631 and 632:
MIL-STD-1797AAPPENDIX Aand make air
Page 633 and 634:
MIL-STD-1797AAPPENDIX Aof high α d
Page 635 and 636:
MIL-STD-1797AAPPENDIX Asimulation o
Page 637 and 638:
MIL-STD-1797AAPPENDIX A4.8.4.2.2 St
Page 639 and 640:
MIL-STD-1797AAPPENDIX A4.8.4.2.3 St
Page 641 and 642:
Page 643 and 644:
MIL-STD-1797AAPPENDIX A4.8.4.2.4 On
Page 645 and 646:
MIL-STD-1797AAPPENDIX A4.8.4.3 Post
Page 647 and 648:
Page 649 and 650:
MIL-STD-1797AAPPENDIX A4.8.4.3.1 De
Page 651 and 652:
MIL-STD-1797AAPPENDIX Amight influe
Page 653 and 654:
Page 655 and 656:
MIL-STD-1797AAPPENDIX AThe AFWAL-TR
Page 657 and 658:
MIL-STD-1797AAPPENDIX A4.8.4.3.2 Re
Page 659 and 660:
Page 661 and 662:
MIL-STD-1797AAPPENDIX AThe low mode
Page 663 and 664:
Page 665 and 666:
MIL-STD-1797AAPPENDIX ATABLE LIII.
Page 667 and 668:
MIL-STD-1797AAPPENDIX AAt low altit
Page 669 and 670:
MIL-STD-1797AAPPENDIX AHoh et al. (
Page 671 and 672:
MIL-STD-1797AAPPENDIX A4.9.2 Defini
Page 673 and 674:
MIL-STD-1797AAPPENDIX ATABLE LIV. D
Page 675 and 676:
MIL-STD-1797AAPPENDIX Aa. Turbulenc
Page 677 and 678:
MIL-STD-1797AAPPENDIX A3. Low-altit
Page 679 and 680:
MIL-STD-1797AAPPENDIX Ae. GustsDisc
Page 681 and 682:
MIL-STD-1797AAPPENDIX Ac. Periodic
Page 683 and 684:
MIL-STD-1797AAPPENDIX AThis require
Page 685 and 686:
MIL-STD-1797AAPPENDIX AThe two most
Page 687 and 688:
MIL-STD-1797AAPPENDIX AA survey of
Page 689 and 690:
MIL-STD-1797AAPPENDIX ATABLE LVI. A
Page 691 and 692:
MIL-STD-1797AAPPENDIX A5.9.2 Defini
Page 693 and 694:
Page 695 and 696:
MIL-STD-1797AAPPENDIX BDETERMINING
Page 697 and 698:
MIL-STD-1797AAPPENDIX BThese envelo
Page 699 and 700:
MIL-STD-1797AAPPENDIX BFIGURE 272.
Page 701 and 702:
MIL-STD-1797AAPPENDIX B687
Page 703 and 704:
MIL-STD-1797AAPPENDIX CThe framewor
Page 705 and 706:
MIL-STD-1797AAPPENDIX CAdditional i
Page 707 and 708:
MIL-STD-1797AAPPENDIX CVerification
Page 709 and 710:
MIL-STD-1797AAPPENDIX CMIL-F-8785C
Page 711 and 712:
Page 713 and 714:
Page 715 and 716:
Page 717:
STANDARDIZATION DOCUMENT IMPROVEMEN
show all

FLYING QUALITIES OF PILOTED AIRCRAFT - CAFE Foundation

Create successful ePaper yourself

Delete template?

Save as template?