FLYING QUALITIES OF PILOTED AIRCRAFT - CAFE Foundation

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MIL–STD–1797AAPPENDIX AFIGURE 161. Flight phase Category A data, moderate |φ/β| d (fromAFFDL–TR–67–98).FIGURE 162. Flight phase Category A data, large and small |φ/β| d (fromAFFDL–TR–67–98).412
MIL–STD–1797AAPPENDIX AFIGURE 163. Flight phase Category B data (from NASA–CR–778).FIGURE 164. Flight phase Category B data (from WADD–TR–61–147).413
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NOTE: MIL-STD-1797A has been redesi
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MIL-STD-1797AFOREWORDThis standard
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MIL-STD-1797ACONTENTS - ContinuedPa
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MIL-STD-1797A1. SCOPE1.1 Purpose. T
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MIL-STD-1797AT 2 Time to double amp
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MIL-STD-1797AV end Speed for maximu
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MIL-STD-1797Aω spUndamped natural
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MIL-STD-1797Awhere p , p and p are
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MIL-STD-1797AFIGURE 1. Roll-sidesli
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MIL-STD-1797AFIGURE 2. Roll-sidesli
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MIL-STD-1797AExamples showing measu
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MIL-STD-1797Aσ, RMS Root-mean-squa
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MIL-STD-1797A4. REQUIREMENTS4.1 Gen
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MIL-STD-1797Athe selected configura
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MIL-STD-1797Ab. For these calculati
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MIL-STD-1797Aindicate to the pilot
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MIL-STD-1797Aaccessibly located, co
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MIL-STD-1797ATABLE IV. Pitch trim c
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MIL-STD-1797Aspeed range by the mos
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MIL-STD-1797Ato designated flight p
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MIL-STD-1797Ainputs are simple, eas
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MIL-STD-1797ARight yaw-control-peda
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MIL-STD-1797Ad. Yaw axis control po
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MIL-STD-1797ADuring combat-type man
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MIL-STD-1797A4.9 Flying qualities r
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MIL-STD-1797A5. VERIFICATION5.1 Gen
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MIL-STD-1797A5.1.12.4 Rate of contr
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MIL-STD-1797A5.2.8.6.5 Pitch axis c
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MIL-STD-1797A5.5.9.3 Roll axis cont
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MIL-STD-1797A5.8 Flying qualities r
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MIL-STD-1797A1st Tier References2nd
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MIL-STD-1797AAPPENDIX AFLYING QUALI
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MIL-STD-1797AAPPENDIX AASD-TDR-63-3
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MIL-STD-1797AAPPENDIX AAFFDL-TR-70-
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MIL-STD-1797AAPPENDIX AAFWAL-TR-81-
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MIL-STD-1797AAPPENDIX AFAA-RD-70-65
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MIL-STD-1797AAPPENDIX ANASA-TM-X-62
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MIL-STD-1797AAPPENDIX AAIAA Paper 6
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MIL-STD-1797AAPPENDIX ABoeing D6-10
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MIL-STD-1797AAPPENDIX AAGARD-CP-333
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MIL-STD-1797AAPPENDIX ANeal, T. Pet
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MIL-STD-1797AAPPENDIX AFor military
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MIL-STD-1797AAPPENDIX AFIGURE 3. Cl
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MIL-STD-1797AAPPENDIX Ab. Cruise (C
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MIL-STD-1797AAPPENDIX AWhile the or
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MIL-STD-1797AAPPENDIX A3.3 Levels a
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MIL-STD-1797AAPPENDIX AFractional r
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MIL-STD-1797AAPPENDIX A40. REQUIREM
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MIL-STD-1797AAPPENDIX AREQUIREMENT
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MIL-STD-1797AAPPENDIX AVERIFICATION
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MIL-STD-1797AAPPENDIX ASome Flight
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MIL-STD-1797AAPPENDIX ATABLE I. Ope
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MIL-STD-1797AAPPENDIX AIf design tr
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MIL-STD-1797AAPPENDIX Ac. The speed
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MIL-STD-1797AAPPENDIX A4.1.4.3 Perm
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MIL-STD-1797AAPPENDIX A4.1.5 Config
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MIL-STD-1797AAPPENDIX A4.1.6 Aircra
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MIL-STD-1797AAPPENDIX A4.1.7.1 Allo
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MIL-STD-1797AAPPENDIX Aart can supp
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MIL-STD-1797AAPPENDIX ATABLE VIII.
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MIL-STD-1797AAPPENDIX AP(Level 2) =
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MIL-STD-1797AAPPENDIX ASee also REQ
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MIL-STD-1797AAPPENDIX Ademonstrated
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MIL-STD-1797AAPPENDIX A4.1.7.4 Gene
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MIL-STD-1797AAPPENDIX A5.1.7.4 Gene
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MIL-STD-1797AAPPENDIX A4.1.7.6 Fail
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MIL-STD-1797AAPPENDIX A4.1.10 Inter
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MIL-STD-1797AAPPENDIX A4.1.11.2 Rel
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MIL-STD-1797AAPPENDIX A4.1.11.4 Fai
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MIL-STD-1797AAPPENDIX ATABLE IX. Su
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MIL-STD-1797AAPPENDIX A4.1.11.5 Con
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MIL-STD-1797AAPPENDIX Aone must con
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MIL-STD-1797AAPPENDIX AUnless deact
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MIL-STD-1797AAPPENDIX ATABLE X. Con
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MIL-STD-1797AAPPENDIX A4.1.11.6 Pil
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MIL-STD-1797AAPPENDIX A4.1.11.7 Res
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While some functions that might be
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MIL-STD-1797AAPPENDIX A4.1.12.4 Rat
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LevelMIL-STD-1797AAPPENDIX ATABLE X
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MIL-STD-1797AAPPENDIX Athunderstorm
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MIL-STD-1797AAPPENDIX AThe irrevers
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MIL-STD-1797AAPPENDIX A4.2 Flying q
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MIL-STD-1797AAPPENDIX Achanges sign
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MIL-STD-1797AAPPENDIX A4.2.1.2 Shor
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MIL-STD-1797AAPPENDIX Apilot pitch
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THE EQUIVALENT SYSTEMS CONCEPTMIL-S
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MIL-STD-1797AAPPENDIX AIt is assume
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MIL-STD-1797AAPPENDIX AThe problem
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MIL-STD-1797AAPPENDIX AFIGURE 15. E
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MIL-STD-1797AAPPENDIX AFIGURE 16. C
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MIL-STD-1797AAPPENDIX AFIGURE 19. P
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MIL-STD-1797AAPPENDIX AFor many air
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MIL-STD-1797AAPPENDIX AFIGURE 22. T
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MIL-STD-1797AAPPENDIX AFIGURE 24. R
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MIL-STD-1797AAPPENDIX AThe last fac
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MIL-STD-1797AAPPENDIX AShort-period
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MIL-STD-1797AAPPENDIX AFIGURE 36. A
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MIL-STD-1797AAPPENDIX Aimposed on l
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MIL-STD-1797AAPPENDIX ALAHOS data (
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C. Transient peak ratio, rise time,
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MIL-STD-1797AAPPENDIX Acriteria do
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MIL-STD-1797AAPPENDIX AThe AFFDL-TR
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MIL-STD-1797AAPPENDIX AD. Bandwidth
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MIL-STD-1797AAPPENDIX AFIGURE 58. S
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MIL-STD-1797AAPPENDIX AFIGURE 59. D
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MIL-STD-1797AAPPENDIX AE. Closed-Lo
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MIL-STD-1797AAPPENDIX AThe criteria
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MIL-STD-1797AAPPENDIX AConfiguratio
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MIL-STD-1797AAPPENDIX AFIGURE 76. H
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MIL-STD-1797AAPPENDIX A* Pitch rate
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MIL-STD-1797AAPPENDIX APHASE LAGFor
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MIL-STD-1797AAPPENDIX Ahorizontal t
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MIL-STD-1797AAPPENDIX Aa. AnalysisA
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MIL-STD-1797AAPPENDIX ACare must be
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MIL-STD-1797AAPPENDIX AFIGURE 89a.
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MIL-STD-1797AAPPENDIX A4.2.2 Pilot-
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MIL-STD-1797AAPPENDIX Afeature at t
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MIL-STD-1797AAPPENDIX AThe correspo
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MIL-STD-1797AAPPENDIX AωBWτ p= 1.
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MIL-STD-1797AAPPENDIX A275
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MIL-STD-1797AAPPENDIX A4.2.5 Pitch
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4.2.6. Pitch axis response to other
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MIL-STD-1797AAPPENDIX A4.2.6.2 Pitc
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MIL-STD-1797AAPPENDIX A5.2.7.2.1 Lo
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MIL-STD-1797AAPPENDIX AFIGURE 96. N
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MIL-STD-1797AAPPENDIX AIt must be s
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MIL-STD-1797AAPPENDIX ATABLE XVII.
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MIL-STD-1797AAPPENDIX AFIGURE 100.
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MIL-STD-1797AAPPENDIX Aratings show
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MIL-STD-1797AAPPENDIX AAccording to
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MIL-STD-1797AAPPENDIX A[The Citabri
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MIL-STD-1797AAPPENDIX AFor a revers
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MIL-STD-1797AAPPENDIX Arequirements
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MIL-STD-1797AAPPENDIX ASome additio
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MIL-STD-1797AAPPENDIX ATABLE XVIII.
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MIL-STD-1797AAPPENDIX AGiven some v
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MIL-STD-1797AAPPENDIX A4.2.8.6.2 Pi
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4.3.1 Flight path response to attit
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MIL-STD-1797AAPPENDIX ATABLE XXIII.
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MIL-STD-1797AAPPENDIX A4.3.1.2 Stea
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MIL-STD-1797AAPPENDIX Adγdδe γ
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Page 377 and 378: MIL-STD-1797AAPPENDIX ACombinations
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MIL-STD-1797AAPPENDIX A4.5.8.3 Roll
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MIL-STD-1797AAPPENDIX AThe third sk
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MIL-STD-1797AAPPENDIX AThe LATHOS r
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MIL-STD-1797AAPPENDIX Apound). It c
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MIL-STD-1797AAPPENDIX A4.5.9.5.2 Ro
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MIL-STD-1797AAPPENDIX AIt should al
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MIL-STD-1797AAPPENDIX AIn the fligh
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MIL-STD-1797AAPPENDIX AIt has long
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MIL-STD-1797AAPPENDIX AAn evaluatio
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MIL-STD-1797AAPPENDIX A4.6.1.3 Wing
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MIL-STD-1797AAPPENDIX AThe bandwidt
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MIL-STD-1797AAPPENDIX AConfiguratio
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MIL-STD-1797AAPPENDIX Arestraint wi
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MIL-STD-1797AAPPENDIX ATABLE XLIII.
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MIL-STD-1797AAPPENDIX ASUPPORTING D
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MIL-STD-1797AAPPENDIX AP-3B (Class
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MIL-STD-1797AAPPENDIX AThe ability
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MIL-STD-1797AAPPENDIX AFor augmente
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MIL-STD-1797AAPPENDIX AHowever, bef
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C. r o/po Near ZeroMIL-STD-1797AAPP
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MIL-STD-1797AAPPENDIX AD. Complex R
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MIL-STD-1797AAPPENDIX A7. If 0.03 <
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MIL-STD-1797AAPPENDIX A4.6.4 Yaw ax
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MIL-STD-1797AAPPENDIX Aand the time
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MIL-STD-1797AAPPENDIX AβC nδa C C
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MIL-STD-1797AAPPENDIX A4.6.5.2. Yaw
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MIL-STD-1797AAPPENDIX A4.6.6 Yaw ax
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MIL-STD-1797AAPPENDIX A4.6.6.3 Yaw
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MIL-STD-1797AAPPENDIX AC yβCβ0δa
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MIL-STD-1797AAPPENDIX Ato augment Y
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MIL-STD-1797AAPPENDIX AUse of such
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in terms of the uncoupled approxima
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MIL-STD-1797AAPPENDIX AMultiaxis, n
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MIL-STD-1797AAPPENDIX ATABLE LI. Di
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MIL-STD-1797AAPPENDIX AA critical d
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MIL-STD-1797AAPPENDIX Aand make air
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MIL-STD-1797AAPPENDIX Aof high α d
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MIL-STD-1797AAPPENDIX Asimulation o
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MIL-STD-1797AAPPENDIX A4.8.4.2.2 St
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MIL-STD-1797AAPPENDIX A4.8.4.2.3 St
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MIL-STD-1797AAPPENDIX A4.8.4.2.4 On
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MIL-STD-1797AAPPENDIX A4.8.4.3 Post
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MIL-STD-1797AAPPENDIX A4.8.4.3.1 De
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MIL-STD-1797AAPPENDIX Amight influe
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MIL-STD-1797AAPPENDIX AThe AFWAL-TR
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MIL-STD-1797AAPPENDIX A4.8.4.3.2 Re
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MIL-STD-1797AAPPENDIX AThe low mode
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MIL-STD-1797AAPPENDIX ATABLE LIII.
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MIL-STD-1797AAPPENDIX AAt low altit
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MIL-STD-1797AAPPENDIX AHoh et al. (
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MIL-STD-1797AAPPENDIX A4.9.2 Defini
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MIL-STD-1797AAPPENDIX ATABLE LIV. D
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MIL-STD-1797AAPPENDIX Aa. Turbulenc
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MIL-STD-1797AAPPENDIX A3. Low-altit
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MIL-STD-1797AAPPENDIX Ae. GustsDisc
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MIL-STD-1797AAPPENDIX Ac. Periodic
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MIL-STD-1797AAPPENDIX AThis require
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MIL-STD-1797AAPPENDIX AThe two most
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MIL-STD-1797AAPPENDIX AA survey of
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MIL-STD-1797AAPPENDIX ATABLE LVI. A
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MIL-STD-1797AAPPENDIX A5.9.2 Defini
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MIL-STD-1797AAPPENDIX BDETERMINING
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MIL-STD-1797AAPPENDIX BThese envelo
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MIL-STD-1797AAPPENDIX BFIGURE 272.
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MIL-STD-1797AAPPENDIX B687
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MIL-STD-1797AAPPENDIX CThe framewor
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MIL-STD-1797AAPPENDIX CAdditional i
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MIL-STD-1797AAPPENDIX CVerification
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MIL-STD-1797AAPPENDIX CMIL-F-8785C
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