An in-flight simulation of VTOL hover control concepts

Corliss, L. D.; Greif, R. K.; Gerdes, R. M.

doi:10.2514/6.1977-610

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1986

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“…Deceleration authority was of no concern. The XV-5A had a limited acceleration capability in transition due to limited thrust, a complex angle-of-attack schedule, and a slow thrust deflection rate' 12 '. Accelerations of 0-13 g were observed during operational experience.…”

Section: Transitionmentioning

confidence: 99%

Control of V/STOL aircraft

Franklin

1986

Aeronaut. j.

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SummaryThis paper deals with control of V/STOL aircraft in powered-lift flight. A review of representative operational mission tasks is presented for the take-off, transition, hover and landing flight phases. Characteristics inherent in the basic airframe and propulsion system and the behaviour associated with control augmentation systems are considered. Demands for augmented stability and control response to meet certain mission operational requirements are discussed. Experience from ground-based simulation and flight experiments that illustrates the impact of augmented stability and control on aircraft design is related by example.

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Section: Transitionmentioning

confidence: 99%

Control of V/STOL aircraft

Franklin

1986

Aeronaut. j.

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An in-flight simulation of VTOL hover control concepts

Cited by 1 publication

References 1 publication

Control of V/STOL aircraft

Control of V/STOL aircraft

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