1997
DOI: 10.1080/002071797222993
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Flight control for mixed-amplitude commands

Abstract: A longitudinal¯ight control law is derived that provides desirable precision aircraft-tracking response for small-amplitude commands and desirable gross acquisition response for large-amplitude commands. Dynamic inversion and proportional-plus-integral command compensation provide precision attitudetracking control, and time-optimal control provides gross acquisition augmentation. Continuous transition between the control modes, without control power saturation, is accomplished using Lyapunov function level se… Show more

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Cited by 7 publications
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References 13 publications
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