Using linear-optimal estimation and control techniques, digital-adaptive control laws have been designed for a tandem-rotor helicopter which is equipped for fully automatic flight in terminal area operations. Two distinct discrete-time control laws are designed to interface with velocity-command and attitude-command guidance logic, and each incorporates proportional-integral compensation for nonzero-set-point regulation, as well as reduced-order Kalman filters for sensor blending and noise rejection. Adaptation to flight condition is achieved with a novel gain-scheduling method based on correlation and regression analysis. The linear-optimal design approach is found to be a valuable tool in the development of practical multivariable control laws for vehicles which evidence significant coupling and insufficient natural stability.
Digital controllers for VTOL aircraft
Digitale Regelungen fuer Senkrechtstarter
IEEE Transactions on Aerospace and Electronic Systems ; 14 , 1 ; 54-63
1978
10 Seiten, 8 Bilder, 8 Quellen
Article (Journal)
English
Digital Controllers for VTOL Aircraft
IEEE | 1978
|Minimum sensitivity controllers with application to VTOL aircraft
Tema Archive | 1980
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