DocumentCode
1619232
Title
Dual-rate global digital redesign for flight control
Author
Rabbath, C.A. ; Hori, N.
Author_Institution
Defence Res. & Dev. Canada, Canada
Volume
1
fYear
2004
Firstpage
338
Abstract
This paper proposes a dual-rate global digital redesign method for the design of flight control systems. Given a two-loop continuous-time autopilot, dual-rate digital redesign based on the concept of plant-input-mapping is applied at each operating point. The proposed approach allows to constrain the orders of the discrete-time controllers, which is a significant consideration when gain scheduling of the linear control laws is performed over the flight envelope. The dual-rate digital redesign technique provides satisfactory closed-loop performances over an extended range of sampling rates, as compared with other widely used methods of digital redesign. Numerical simulations of a symmetrical, tail-controlled missile demonstrate the effectiveness of the proposed method.
Keywords
aerospace control; closed loop systems; continuous time systems; discrete time systems; linear systems; closed-loop performance; discrete-time controllers; dual-rate global digital redesign; flight control system; linear control laws; tail-controlled missile;
fLanguage
English
Publisher
ieee
Conference_Titel
SICE 2004 Annual Conference
Conference_Location
Sapporo
Print_ISBN
4-907764-22-7
Type
conf
Filename
1491422
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