Control of nearly Singular Decoupling Systems and nonlinear Aircraft Maneuver
Document Type
Article
Publication Date
11-1988
Publication Title
IEEE Transactions on Aerospace and Electronic Systems
Volume
24
First page number:
775
Last page number:
784
Abstract
The author treats the question of control of a class of nonlinear systems using state variable feedback whose input/output map is nearly singular. Although the existing decoupling theory is applicable to such systems, this requires a large amount of control, which may not be permissible. A decoupling approach using state variable feedback in an approximate sense, but requiring a small control magnitude is considered. A decoupling scheme is presented that gives rise to a singularly perturbed system describing the fast dynamics of the control vector. The quasi-steady-state solution of the system gives a control law that decouples the system in an approximate way. The controller includes a servo compensator and a reference trajectory generator. Based on this result, a control law for approximate decoupling of roll angle, angle of attack, and sideslip in rapid, nonlinear airplane maneuvers is derived. Simulated responses of the closed-loop system show that large, simultaneous lateral and longitudinal maneuvers can be accurately performed in spite of uncertainty in stability derivatives.
Keywords
Aerospace control; Aircraft; Airplanes; Control system synthesis; Control systems; Electric variables control; Force control; Nonlinear control systems; Nonlinear systems; State feedback
Disciplines
Aeronautical Vehicles | Aerospace Engineering | Astrodynamics | Controls and Control Theory | Electrical and Computer Engineering | Electrical and Electronics | Electronic Devices and Semiconductor Manufacturing | Multi-Vehicle Systems and Air Traffic Control | Navigation, Guidance, Control and Dynamics | Power and Energy | Propulsion and Power | Signal Processing | Structures and Materials | Systems Engineering and Multidisciplinary Design Optimization
Language
English
Permissions
Use Find in Your Library, contact the author, or interlibrary loan to garner a copy of the item. Publisher policy does not allow archiving the final published version. If a post-print (author's peer-reviewed manuscript) is allowed and available, or publisher policy changes, the item will be deposited.
Repository Citation
Singh, S. N.
(1988).
Control of nearly Singular Decoupling Systems and nonlinear Aircraft Maneuver.
IEEE Transactions on Aerospace and Electronic Systems, 24
775-784.