Passive homing missile guidance law based on new target maneuver models
- 1 September 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 13 (5) , 803-812
- https://doi.org/10.2514/3.25405
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Suboptimal filter design with pseudomeasurements for target trackingIEEE Transactions on Aerospace and Electronic Systems, 1988
- A stochastic analysis of a modified gain extended Kalman filter with applications to estimation with bearings only measurementsIEEE Transactions on Automatic Control, 1985
- Target acceleration modeling for tactical missile guidanceJournal of Guidance, Control, and Dynamics, 1984
- Application of state estimation to target trackingIEEE Transactions on Automatic Control, 1984
- Estimation and prediction for maneuvering target trajectoriesIEEE Transactions on Automatic Control, 1983
- Linear minimum variance filters applied to carrier trackingIEEE Transactions on Automatic Control, 1976
- An approximation method for estimation in linear systems with parameter uncertaintyIEEE Transactions on Automatic Control, 1975