Aircraft Handling Qualities and Pilot-Induced Oscillation Tendencies with Actuator Saturation
- 1 November 1999
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 22 (6) , 852-861
- https://doi.org/10.2514/2.4463
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Assessing Aircraft Susceptibility to Nonlinear Aircraft-Pilot Coupling/Pilot-Induced OscillationsJournal of Guidance, Control, and Dynamics, 1998
- Unified Theory for Aircraft Handling Qualities and Adverse Aircraft-Pilot CouplingJournal of Guidance, Control, and Dynamics, 1997
- A Limited Flight Test Investigation of Pilot-Induced Oscillation Due to Elevator Rate Limiting (HAVE LIMITS)Published by Defense Technical Information Center (DTIC) ,1997