Missile Guidance Laws Based on Singular Perturbation Methodology
- 1 March 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance and Control
- Vol. 3 (2), 158-165
- https://doi.org/10.2514/3.55964
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- The closed-form solution of true proportional navigationIEEE Transactions on Aerospace and Electronic Systems, 1976
- Singular perturbations and order reduction in control theory — An overviewAutomatica, 1976
- Quasi-optimum proportional navigationIEEE Transactions on Automatic Control, 1970
- Proportional Navigation on Nonstationary TargetsIEEE Transactions on Aerospace and Electronic Systems, 1970
- Fundamentals of proportional navigationIEEE Spectrum, 1966