Multi-constraint Guidance Law Design for Asymmetric Vision with Side Window Detection

In addressing the challenge of precision strike targeting under the constraints of asymmetric visual fields during side window detection, this paper introduces a novel multi-constraint guidance law. This law takes into account the asymmetry of the field of view, encompassing attack angles and desired engagement times. Initially, a mathematical model is developed to represent three-dimensional space constraints within the side window. The study then transitions to a two-dimensional space in the longitudinal plane, establishing the guidance relationship between the missile and the target. Building upon a generalized optimal attack angle guidance law, the attack time error is chosen as the tracking error metric, leading to the derivation of a time-angle constrained guidance law through optimal error dynamics. Furthermore, the constraints of the asymmetric field of view of the seeker under side window detection are considered, analyzing how each element of the guidance law impacts the field of view angle. Utilizing various limiting functions, the distance at which the missile loses the target is substantially reduced. Mathematical simulations confirm the effectiveness of the designed guidance law in addressing the problem of guidance within the context of side window detection.