Analysis of Aircraft Attitude Control Systems Prone to Pilot-Induced Oscillations
- 1 January 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 7 (1) , 106-112
- https://doi.org/10.2514/3.56363
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- In-Flight Evaluation of Control System Pure Time DelaysJournal of Aircraft, 1982
- An Adaptive Stick-Gain to Reduce Pilot-Induced Oscillation TendenciesJournal of Guidance, Control, and Dynamics, 1982
- Flight Tests of a Microprocessor Control SystemJournal of Guidance and Control, 1980
- A Design Procedure for Control/Display SystemsHuman Factors: The Journal of the Human Factors and Ergonomics Society, 1977
- An In-Flight Investigation to Develop Control System Design Criteria for Fighter Airplanes. Volume 1Published by Defense Technical Information Center (DTIC) ,1970
- An optimal control model of human response part I: Theory and validationAutomatica, 1970
- THE THEORY AND APPLICATION OF LINEAR OPTIMAL CONTROLPublished by Defense Technical Information Center (DTIC) ,1966
- HUMAN PILOT DYNAMICS IN COMPENSATORY SYSTEMSPublished by Defense Technical Information Center (DTIC) ,1965