TY - GEN
T1 - Varying-Gain Proportional Navigation Guidance Law for Precise Impact Time and Angle Control
AU - Wang, Chenxing
AU - Zhang, Yuchen
AU - Wang, Pengyu
AU - Yang, Yuxin
AU - Lv, Yueyong
AU - Guo, Yanning
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - This paper introduces a novel varying-gain proportional navigation guidance (PNG) law for driving constantspeed missiles to achieve desired impact angles on stationary targets. The unique advantage of the proposed varying-gain PNG law lies in its ability to provide accurate, analytical time-to-go estimations across a broad feasible region, which facilitate the precise control of impact time. To show the significance of our new method, the proposed varying-gain PNG law is augmented with a biased feedback command to obtain an impact time and angle control guidance (ITACG) law. Numerical simulations, in comparison with existing methods, demonstrate that both the proposed varying-gain PNG and ITACG laws can achieve desired impact constraints while requiring less control effort, even under conditions of large initial heading errors and stringent impact angle constraints.
AB - This paper introduces a novel varying-gain proportional navigation guidance (PNG) law for driving constantspeed missiles to achieve desired impact angles on stationary targets. The unique advantage of the proposed varying-gain PNG law lies in its ability to provide accurate, analytical time-to-go estimations across a broad feasible region, which facilitate the precise control of impact time. To show the significance of our new method, the proposed varying-gain PNG law is augmented with a biased feedback command to obtain an impact time and angle control guidance (ITACG) law. Numerical simulations, in comparison with existing methods, demonstrate that both the proposed varying-gain PNG and ITACG laws can achieve desired impact constraints while requiring less control effort, even under conditions of large initial heading errors and stringent impact angle constraints.
KW - impact angle control
KW - impact time control
KW - proportional navigation guidance
KW - time-to-go estimation
UR - https://www.scopus.com/pages/publications/105013966911
U2 - 10.1109/CCDC65474.2025.11090748
DO - 10.1109/CCDC65474.2025.11090748
M3 - 会议稿件
AN - SCOPUS:105013966911
T3 - Proceedings of the 37th Chinese Control and Decision Conference, CCDC 2025
SP - 4663
EP - 4669
BT - Proceedings of the 37th Chinese Control and Decision Conference, CCDC 2025
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 37th Chinese Control and Decision Conference, CCDC 2025
Y2 - 16 May 2025 through 19 May 2025
ER -