The tracking properties of fast tracking algorithms were considered and analyzed (1-57 assuming a single target in clean and in cluttered environment with various values for probability of detectionCP D. In the present work.we extend our study to tracking environments where typical multi-target tracking cases arise,e.g.,two closely spaced targets Ctypical for a target in formation)and the case of two crossing targets.The obtained the results reveal that with a 100% PD and zero clutter density.perfect data association at smaller targets spacings is provided with fast Kalman filter of order N=2 compared to N=3 for the gradient lattice filter.At higher clutter densities, even with a 100% PD, the fast Kalman filter has shown unstable behavior at target spacings below some threshold values, In case of tracking crossing tracks a nondiverging fast Kalman tracking filter with Nm2 has almost the same capability as a gradient lattice filter having N=4 at various values of P and at various clutter densities. Conditions that guarantee a stable performance of the fast Kalman filter are given.
Hamad, A., Yousef, S., Matar, M., & Nofal, H. (1991). Performance of Fast Algorithms of Multi-target Tracking. International Conference on Aerospace Sciences and Aviation Technology, 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO), 505-514. doi: 10.21608/asat.1991.25833
MLA
A. M. Hamad; S. Yousef; M. A. Matar; H. Nofal. "Performance of Fast Algorithms of Multi-target Tracking", International Conference on Aerospace Sciences and Aviation Technology, 4, ASAT CONFLENCE 14-16 May 1991 , CAIRO, 1991, 505-514. doi: 10.21608/asat.1991.25833
HARVARD
Hamad, A., Yousef, S., Matar, M., Nofal, H. (1991). 'Performance of Fast Algorithms of Multi-target Tracking', International Conference on Aerospace Sciences and Aviation Technology, 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO), pp. 505-514. doi: 10.21608/asat.1991.25833
VANCOUVER
Hamad, A., Yousef, S., Matar, M., Nofal, H. Performance of Fast Algorithms of Multi-target Tracking. International Conference on Aerospace Sciences and Aviation Technology, 1991; 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO): 505-514. doi: 10.21608/asat.1991.25833