Title :
Missile Altitude Adaptive Control: A Case Study
Author :
Duque, M. ; Landau, L. ; M´Saad, M. ; Manguin, B. ; Houdement, J. ; Martin, A.
Author_Institution :
Laboratoire d´´Automatique de Grenoble, U.A. C.N.R.S. 228 E.N.S.I.E.G. - I.N.P.G., B.P.46 -38402 St- Martin d´´Hÿres, France
Abstract :
This paper presents some missile attack angle control simulation studies. Both linear and adaptive control are considered using the partial state model reference adaptive control approach proposed in [1]. The main control problems are due to the unmeasured disturbances, unstable or undamped modes and important dynamics variations.
Keywords :
Adaptive control; Computer aided software engineering; Context modeling; Control design; Missiles; Polynomials; Predictive control; Predictive models; Programmable control; Rockets; Partial state model reference control; adaptive control; generalized predictive control; missile altitude control; robust parameter estimator;
Conference_Titel :
American Control Conference, 1989
Conference_Location :
Pittsburgh, PA, USA
