TY - JOUR
T1 - 3-D Integrated Guidance and Control for Strapdown Interceptor under Divert and Attitude Control System
AU - Peng, Qian
AU - Li, Bo
AU - Guo, Jianguo
AU - Guo, Zongyi
N1 - Publisher Copyright:
© 1965-2011 IEEE.
PY - 2026
Y1 - 2026
N2 - A 3-D integrated guidance and control (IGC) law for divert and attitude control system (DACS)-based strapdown interceptor subjected to strong couplings and complex constraints is proposed in this article. The 3-D kinematic and dynamic equations reflecting the couplings of the interceptor are constructed by combining the characteristics of DACS and strapdown seeker. An improved IGC model is established by employing the proposed adaptive fixed-time prescribed performance function (AFTPPF). This model takes into account the boundary, terminal, and convergence time constraints of strapdown interceptor, along with the mismatched unknown uncertainties. An IGC law is developed within the high-order multidimensional sliding mode control framework, integrating the AFTPPF to handle the complex constrains without computational singularities and the extended disturbance observer for uncertainty estimations. Finally, the stability and performance of the proposed control method are proved.
AB - A 3-D integrated guidance and control (IGC) law for divert and attitude control system (DACS)-based strapdown interceptor subjected to strong couplings and complex constraints is proposed in this article. The 3-D kinematic and dynamic equations reflecting the couplings of the interceptor are constructed by combining the characteristics of DACS and strapdown seeker. An improved IGC model is established by employing the proposed adaptive fixed-time prescribed performance function (AFTPPF). This model takes into account the boundary, terminal, and convergence time constraints of strapdown interceptor, along with the mismatched unknown uncertainties. An IGC law is developed within the high-order multidimensional sliding mode control framework, integrating the AFTPPF to handle the complex constrains without computational singularities and the extended disturbance observer for uncertainty estimations. Finally, the stability and performance of the proposed control method are proved.
KW - 3-D integrated guidance and control (IGC)
KW - divert and attitude control system (DACS)
KW - prescribed performance function (PPF)
KW - strapdown interceptor
UR - https://www.scopus.com/pages/publications/105035411490
U2 - 10.1109/TAES.2026.3681889
DO - 10.1109/TAES.2026.3681889
M3 - 文章
AN - SCOPUS:105035411490
SN - 0018-9251
VL - 62
SP - 9331
EP - 9344
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
ER -