Robust, Decoupled, Flight Control Design with Rate-Saturating Actuators
- 1 May 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 21 (3) , 361-367
- https://doi.org/10.2514/2.4253
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Unified Theory for Aircraft Handling Qualities and Adverse Aircraft-Pilot CouplingJournal of Guidance, Control, and Dynamics, 1997
- Approximations for Quantitative Feedback Theory DesignsJournal of Guidance, Control, and Dynamics, 1997
- Flight Control System Design with Rate Saturating ActuatorsJournal of Guidance, Control, and Dynamics, 1997
- Pilot-Induced Oscillation Analysis and Prediction with Actuator Rate LimitingJournal of Guidance, Control, and Dynamics, 1997
- MIMO QFT using non-diagonal controllersInternational Journal of Control, 1995
- Dynamic inversion: an evolving methodology for flight control designInternational Journal of Control, 1994
- Multi‐input, multi‐output flight control system design for the YF‐16 using nonlinear QFT and pilot compensationInternational Journal of Robust and Nonlinear Control, 1994
- Robust crossfeed design for hovering rotorcraftInternational Journal of Robust and Nonlinear Control, 1994
- Invited paper Survey of quantitative feedback theory (QFT)International Journal of Control, 1991
- High performance linear-quadratic and H-infinity designs for a 'supermaneuverable' aircraftJournal of Guidance, Control, and Dynamics, 1991