Linear optimal control for an aircraft model | Zendy

Frangos C. | Zendy

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Linear optimal control for an aircraft model

Author(s) -

Frangos C.

Publication year - 1993

Publication title -

optimal control applications and methods

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.458

H-Index - 44

eISSN - 1099-1514

pISSN - 0143-2087

DOI - 10.1002/oca.4660140406

Subject(s) - weighting , optimal control , control theory (sociology) , diagonal , minification , linear programming , controller (irrigation) , mathematics , full state feedback , linear system , slip (aerodynamics) , mathematical optimization , computer science , control (management) , engineering , mathematical analysis , physics , aerospace engineering , geometry , artificial intelligence , acoustics , agronomy , biology

A linear optimal proportional plus integral (PI) controller is designed for a lateral aircraft model such that an approximately decoupled closed‐loop step response is obtained for the roll angle and side‐slip angle while the linear optimal feedback gains are simultaneously minimized. A standard mathematical programming algorithm is employed to calculate the diagonal state weighting matrix Q such that the specifications are satisfied. The synthesis procedure consists of the iterative minimization of a functional where at each iteration step a linear optimal control problem is solved.

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