Robust Longitudinal Control Design Using Dynamic Inversion and Quantitative Feedback Theory
- 1 September 1997
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 20 (5) , 933-940
- https://doi.org/10.2514/2.4137
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Quantitative feedback theory with a scheduled gain for full envelope longitudinal controlJournal of Guidance, Control, and Dynamics, 1996
- Full envelope flight control system design using quantitative feedback theoryJournal of Guidance, Control, and Dynamics, 1996
- Robust Dynamic Inversion for Control of Highly Maneuverable AircraftJournal of Guidance, Control, and Dynamics, 1995
- Dynamic inversion: an evolving methodology for flight control designInternational Journal of Control, 1994
- Quantitative feedback theory technique and applicationsInternational Journal of Control, 1994
- Quantitative feedback theory applied to the design of a rotorcraft flight control systemJournal of Guidance, Control, and Dynamics, 1993
- Nonlinear inversion flight control for a supermaneuverable aircraftJournal of Guidance, Control, and Dynamics, 1992
- Gain scheduling: potential hazards and possible remediesIEEE Control Systems, 1992
- Nonlinear control law with application to high angle-of-attack flightJournal of Guidance, Control, and Dynamics, 1992
- Improvement in quantitative non-linear feedback design by cancellationInternational Journal of Control, 1981