Title :
Robust control design for aerospace applications
Author :
Yedavalli, Rama K.
Author_Institution :
Ohio State Univ., Columbus, OH, USA
fDate :
5/1/1989 12:00:00 AM
Abstract :
Time-domain control design for stability robustness of linear systems with structured uncertainty is addressed. Upper bounds on the linear perturbation of an asymptotically stable linear system are obtained, making it possible to maintain stability by using the structural information of the uncertainty. A quantitative measure called the stability robustness index is introduced and used to design controllers for robust stability. The proposed state feedback control design algorithm can be used, for a given set of perturbations, to select the range of control effort for which the system is stability-robust. Conversely it can be used, for a given control effort, to determine the size of the tolerable perturbation. The algorithm is illustrated with examples from aircraft control and large-space-structure control problems
Keywords :
aerospace control; aircraft control; control system synthesis; feedback; linear systems; stability; time-domain synthesis; aerospace applications; aircraft control; asymptotically stable linear system; large-space-structure control; linear perturbation; stability robustness; state feedback control design algorithm; structured uncertainty; time domain control; tolerable perturbation; Aerospace control; Asymptotic stability; Control design; Linear systems; Measurement uncertainty; Robust control; Robust stability; State feedback; Time domain analysis; Upper bound;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on