DocumentCode :
2650195
Title :
Spherical target state estimators
Author :
Souza, Christopher N D´ ; McClure, Mark A. ; Cloutier, James R.
Author_Institution :
Navigation and Control Branch, US Air Force Armament Directorate, Eglin AFB, FL, USA
Volume :
2
fYear :
1994
fDate :
29 June-1 July 1994
Firstpage :
1675
Abstract :
A spherical filter formulation is derived and the resulting nonlinear estimator is applied to a tactical air-to-air missile intercept problem. An Extended Kalman filter is used to estimate the target acceleration in the line-of-sight frame. The estimator models the target acceleration as a first-order Gauss-Markov process. A method suggested by Singer was used to select the process noise power spectral density matrix. Next, a kinematic constraint is used to improve the estimated target acceleration by using a fictitious measurement to augment the seeker measurements. Finally, a form of adaptive filtering is used to obtain a better value for the target acceleration time constant. These techniques are evaluated using a representative target engagement scenario.
Keywords :
Gaussian processes; Markov processes; adaptive Kalman filters; kinematics; missile guidance; state estimation; adaptive filtering; extended Kalman filter; first-order Gauss-Markov process; kinematic constraint; line-of-sight frame; noise power spectral density matrix; nonlinear estimator; spherical filter; tactical air-to-air missile intercept; target acceleration estimation; Acceleration; Accelerometers; Filters; Force control; Kinematics; Missiles; Motion estimation; Navigation; Nonlinear equations; State estimation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1994
Print_ISBN :
0-7803-1783-1
Type :
conf
DOI :
10.1109/ACC.1994.752356
Filename :
752356
Link To Document :
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