Pseudorate sawtooth-pulse-reset control system analysis and design.
- 1 June 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 4 (6) , 781-785
- https://doi.org/10.2514/3.28951
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Derived-Rate Increment Stabilization: Its Application to the Attitude Control ProblemJournal of Basic Engineering, 1962