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