TY - JOUR
T1 - Prescribed performance-based guidance law for impact-angle and impact-time control with field-of-view constraints
AU - Mushtaq, Muhammad
AU - Yu, Wenbin
AU - Chen, Wanchun
N1 - Publisher Copyright:
© IMechE 2026
PY - 2026
Y1 - 2026
N2 - This study presents a homing guidance law based on a prescribed performance controller (PPC) to simultaneously satisfy impact-angle and impact-time constraints. The proposed approach leverages a range-parametrized prescribed performance function (PPF) designed to be continuous and smoothly differentiable to enforce the impact-angle constraint. For the impact-time constraint, a closed-form expression for the time-to-go is first derived by modeling the line-of-sight angle as a polynomial function of the range. The resulting time-to-go error dynamics are then enforced through the designed PPF, whose bounds dynamically contract with the remaining range to ensure error convergence to the prescribed terminal bounds. The field-of-view constraint is enforced through a smooth switching function in the integrated guidance law, ensuring that the look-angle remains within its prescribed limits. Extensive numerical simulations validate the effectiveness of the proposed approach.
AB - This study presents a homing guidance law based on a prescribed performance controller (PPC) to simultaneously satisfy impact-angle and impact-time constraints. The proposed approach leverages a range-parametrized prescribed performance function (PPF) designed to be continuous and smoothly differentiable to enforce the impact-angle constraint. For the impact-time constraint, a closed-form expression for the time-to-go is first derived by modeling the line-of-sight angle as a polynomial function of the range. The resulting time-to-go error dynamics are then enforced through the designed PPF, whose bounds dynamically contract with the remaining range to ensure error convergence to the prescribed terminal bounds. The field-of-view constraint is enforced through a smooth switching function in the integrated guidance law, ensuring that the look-angle remains within its prescribed limits. Extensive numerical simulations validate the effectiveness of the proposed approach.
KW - field-of-view constraint
KW - impact-angle control
KW - impact-time control
KW - prescribed performance control
UR - https://www.scopus.com/pages/publications/105039678620
U2 - 10.1177/09544100261451550
DO - 10.1177/09544100261451550
M3 - 文章
AN - SCOPUS:105039678620
SN - 0954-4100
JO - Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
JF - Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
ER -