This paper considers a given set of fixed order compensators for aircraft pitch control problem. By augmenting compensator variables to the original state equations of the aircraft, a new dynamic model is considered to seek a LQ controller. While the fixed order compensators can achieve a set of desired poles in a specified region, LQ formulation provides the inherent robustness properties. The time response for ride quality is significantly improved with a set of dynamic compensators.
Aircraft Pitch Control with Fixed Order LQ Compensators
1997-02-01
Conference paper
No indication
English
Aircraft Pitch Control with Fixed Order LQ Compensators
British Library Conference Proceedings | 1997
|Aircraft Pitch Control With Fixed Order LQ Compensators
NTRS | 1997
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