DocumentCode :
306605
Title :
Decoupling compensation for the Apache helicopter
Author :
Hicks, Kevin L. ; Rodriguez, Armando A.
Author_Institution :
Center for Syst. Sci. & Eng., Arizona State Univ., AZ, USA
Volume :
2
fYear :
1996
fDate :
11-13 Dec 1996
Firstpage :
1551
Abstract :
The design of a decoupling compensator for the Apache helicopter is presented. The design is based on linear quadratic regulation with implicit model following. A decoupling compensator is designed for a reduced-order linear model of vehicle dynamics at hover using eigenstructure assignment. The resulting closed-loop system is used as a reference model in the design of a compensator for the full-order system, resulting in a constant state feedback matrix. A feedforward matrix (command mixer) is then designed to diagonalize the system at low frequencies. The design is evaluated with both the full-order linear model and a nonlinear simulation, ARMCOP. It is found to provide desired bandwidth and good decoupling properties with the linear model. The nonlinear simulation shows increased coupling due to the nonlinearities
Keywords :
aircraft control; closed loop systems; compensation; control system synthesis; dynamics; eigenstructure assignment; helicopters; linear quadratic control; matrix algebra; reduced order systems; state feedback; ARMCOP; Apache helicopter; closed-loop system; command mixer; constant state feedback matrix; decoupling compensation; diagonalization; eigenstructure assignment; feedforward matrix; full-order system; implicit model following; linear quadratic regulation; nonlinear simulation; reduced-order linear model; vehicle dynamics; Aircraft; Automotive engineering; Blades; Design methodology; Engines; Frequency; Helicopters; Nonlinear equations; Shafts; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1996., Proceedings of the 35th IEEE Conference on
Conference_Location :
Kobe
ISSN :
0191-2216
Print_ISBN :
0-7803-3590-2
Type :
conf
DOI :
10.1109/CDC.1996.572743
Filename :
572743
Link To Document :
بازگشت