Paper Info
Title
Brief paper: Short-time parameter optimization with flight control application
Abstract
A design approach is presented for systems operating over a relatively short period of time about various operating points with state variable constraints. This class of problems is especially relevant to certain flight control problems. The design approach is applied to a simplified model of longitudinal dynamics of the F-4 aircraft operating in three widely separated flight conditions. A linear model is assumed about each operating point. Control is achieved via constrained state feedback. The basic problem is then to minimize a suitable integral quadratic performance measure subject to state variable constraints. The main theoretical result is theorem 1 which supplies the inequality constraints required to guarantee short-time stability. The short-time optimization problem is ultimately reduced to a nonlinear programming problem with inequality constraints.
Year
DOI
Venue
1974
10.1016/0005-1098(74)90069-7
Automatica (Journal of IFAC)
Keywords
DocType
Volume
brief paper,Short-time parameter optimization,operating point,inequality constraint,flight control application,short-time optimization problem,certain flight control problem,basic problem,state feedback,design approach,various operating point,F-4 aircraft operating,nonlinear programming problem
Journal
10
Issue
ISSN
Citations 
4
0005-1098
9
PageRank 
References 
Authors
0.54
0
2
Name
Order
Citations
PageRank
Frank A. San Filippo190.54
Peter Dorato216519.52