Development and Comparison of Estimation Algorithms for Airborne Missiles.
Final rept. Dec 81-Dec 82,
MISSISSIPPI STATE UNIV MISSISSIPPI STATE DEPT OF AEROPHYSICS AND AEROSPACE ENGINEERING
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Basic development of the estimation, guidance, and control algorithms for guidance of an airborne missile during air-to-air combat engagements are examined. The extended Kalman filter is improved through the use of sample measurement statistics, through time-weighting the measurements, and through iterating within the Kalman filter. Numerical results are presented for comparing the performance of different filters.
- Theoretical Mathematics
- Computer Hardware
- Air- and Space-Launched Guided Missiles