Synthesis and evaluation of an H2 control law for a hovering helicopter
- 1 May 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 16 (3) , 579-584
- https://doi.org/10.2514/3.21048
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Design of attitude and rate command systems for helicopters using eigenstructure assignmentJournal of Guidance, Control, and Dynamics, 1989
- Eigenstructure Assignment for Linear SystemsIEEE Transactions on Aerospace and Electronic Systems, 1983
- Analytical Design of a High Performance Stability and Control Augmentation System for a Hingeless Rotor HelicopterJournal of the American Helicopter Society, 1979