The paper describes the method of polynomial eigenstructure assignment and its application to a multivariable VSTOL aircraft. The theory of polynomial eigenstructure assignment is described, together with the controller structure. Metrics are described that evaluate interaction, actuator motion and robustness.
Flight control of a VSTOL aircraft using polynomial eigenstructure assignment
1996-01-01
6 pages
Aufsatz (Zeitschrift)
Englisch
robustness , closed loop systems , velocity control , eigenstructure assignment , aircraft control , flight control , controller structure , compensation , polynomial eigenstructure assignment , polynomials , interaction , MIMO systems , poles and zeros , VSTOL aircraft , actuator motion , robust control
Use of eigenstructure assignment in VSTOL aircraft control law design
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