RECOVERY GUIDANCE SATISFYING INPUT AND STATE CONSTRAINTS - RATE SATURATING ACTUATOR EXAMPLE

Authors
Citation
S. Devasia et G. Meyer, RECOVERY GUIDANCE SATISFYING INPUT AND STATE CONSTRAINTS - RATE SATURATING ACTUATOR EXAMPLE, Journal of guidance, control, and dynamics, 21(5), 1998, pp. 733-741
Citations number
23
Categorie Soggetti
Instument & Instrumentation","Aerospace Engineering & Tecnology
ISSN journal
07315090
Volume
21
Issue
5
Year of publication
1998
Pages
733 - 741
Database
ISI
SICI code
0731-5090(1998)21:5<733:RGSIAS>2.0.ZU;2-N
Abstract
When a fixed regulator is used to stabilize a desired state trajectory (guidance law), large initial tracking errors can lead to input satur ation, which can result in performance deterioration. A method to modi fy the guidance law for recovering state-trajectory tracking (without violating input and state constraints) is presented. Although it may b e feasible to find such a satisfactory recovery guidance maneuver for a given initial tracking error, online development of recovery guidanc e maneuvers may not be computationally tractable. A technique Is devel oped to use precomputed recovery guidance maneuvers (precomputed for a finite set of initial tracking errors) to generate recovery guidance maneuvers for other initial errors. The technique is applied to an ill ustrative example with a rate-limited servoactuator, and simulation re sults are presented.