Nonlinear inversion flight control for a supermaneuverable aircraft
- 1 July 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 15 (4) , 976-984
- https://doi.org/10.2514/3.20932
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Nonlinear flight control design via sliding methodsJournal of Guidance, Control, and Dynamics, 1990
- Flight control design using non-linear inverse dynamicsAutomatica, 1988
- Control of nearly singular decoupling systems and nonlinear aircraft maneuverIEEE Transactions on Aerospace and Electronic Systems, 1988
- Nonlinear flight test trajectory controllers for aircraftJournal of Guidance, Control, and Dynamics, 1987
- An interpretation of airplane general motion and contol as inverse problemJournal of Guidance, Control, and Dynamics, 1986
- Future fighter technologiesJournal of Aircraft, 1980
- Two-time-scale feedback design of a class of nonlinear systemsIEEE Transactions on Automatic Control, 1978
- Decoupling of a Class of Nonlinear Systems and Its Application to an Aircraft Control ProblemJournal of Aircraft, 1973
- Decoupling in a Class of Nonlinear Systems by State Variable FeedbackJournal of Dynamic Systems, Measurement, and Control, 1972
- Singular perturbation of linear regulators: Basic theoremsIEEE Transactions on Automatic Control, 1972