초록 ▼

A method of maneuvering target tracing is disclosed. The present invention relates to the field of target tracking and more generally to a method of employing multiple model and variable sampling rate technique, which achieve good tracking performance for a high-g maneuvering target. The results sho

A method of maneuvering target tracing is disclosed. The present invention relates to the field of target tracking and more generally to a method of employing multiple model and variable sampling rate technique, which achieve good tracking performance for a high-g maneuvering target. The results show that the present invention can handle the missile sudden maneuver better and are accurate.

대표청구항 ▼

1. A method of maneuvering target tracking by combining Variable Sampling Rate Technique with Modified Interacting Multiple Model algorithm having the innovation covariance S j(k)=Hj(k)[Pj(k−1 |k|1)+&xgr;j×Qj(k)]Hj(k)T+Rj(k), Sj(k) being the innovation covariance, Hj(k) being the

1. A method of maneuvering target tracking by combining Variable Sampling Rate Technique with Modified Interacting Multiple Model algorithm having the innovation covariance S j(k)=Hj(k)[Pj(k−1 |k|1)+&xgr;j×Qj(k)]Hj(k)T+Rj(k), Sj(k) being the innovation covariance, Hj(k) being the measurement matrix, Pj(k−1 |k−1) being the state prediction covariance, Rj(k) being the measurement noise covariance, &xgr;jis the adaptive factor and Qj(k) is the process noise covariance, comprising the steps of:(a) increasing sampling rate when target is in high-g maneuvering state and increasing adaptive factor &xgr;jto scale up process noise covariance Qj(k) such that the innovation covariance Sj(k) is increased to adapt to the high-g maneuvering state; and(b) decreasing sampling rate when target is in constant speed and decreasing adaptive factor &xgr;jto scale down process noise covariance Qj(k) such that the innovation covariance Sj(k) is decreased to adapt to the constant speed state.2. The method according to claim 1, wherein the normalized innovation and the range rate residual are used to detect target high-g maneuvering state and in turn scale up the adaptive factor &xgr;j.3. A method of maneuvering target tracking by combining Variable Sampling Rate Technique with Interacting Acceleration Compensation algorithm, in bias-free model with innovation covariance S(k)=H(k)[P(k−1 |k−1)+&xgr;×Q(k)]H(k) T+R(k), S(k) being the innovation covariance, H(k) being the measurement matrix, P(k−1 |k−1) being the state prediction covariance, R(k) being the measurement noise covariance, &xgr; being the adaptive factor and Q(k) being the process noise covariance comprising the steps of:(i) increasing sampling rate when target is in high-g maneuvering state and increasing adaptive factor &xgr; to scale up process noise covariance Q(k) such that the innovation covariance S(k) is increased to adapt to the high-g maneuvering state;(ii) decreasing sampling rate when target is in constant speed and decreasing adaptive factor &xgr; to scale down process noise covariance Q(k) such that the innovation covariance S(k) is decreased to adapt to the constant speed state; and(iii) employing normalized innovation and range rate residual to detect target high-g maneuvering state and in turn scale up the adaptive factor &xgr;.4. A method of maneuvering target tracking by combining Variable Sampling Rate Technique with Interacting Acceleration Compensation algorithm in bias model with innovation covariance &Sgr;(k|k−1)=&Sgr;(k−1 |k−1)+&zgr;×G b(k−1) Qb(k−1) Gb(k−1)T, &Sgr;(k|k−1) being the bias model innovation covariance, &zgr; being the adaptive factor and Qb(k−1) being the bias model process noise covariance, comprising the steps of:(i) increasing sampling rate when target is in high-g maneuvering state and increasing adaptive factor &zgr; to scale up process noise covariance. Qb(k−1) such that the innovation covariance &Sgr;(k|k−1) is increased to adapt to the high-g maneuvering state;(ii) decreasing sampling rate when target is in constant speed and decreasing adaptive factor &zgr; to scale down process noise covariance Qb(k−1) such that the innovation covariance &Sgr;(k|k−1) is decreased to adapt to the constant speed state; and(iii) employing normalized innovation and range rate residual to detect target high-g maneuvering state and in turn scale up the adaptive factor &zgr;.