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1 mar 2020 · In this paper, a novel 3D guidance law is proposed to control both the impact time and angle based on computational geometry. LASCs are introduced in the trajectory design. The impact angle is achieved by making the missile travel along the collision line.
30 sty 2021 · This paper proposed an optimal time-varying proportional navigation guidance law based on sequential convex programming. The guidance law can achieve the desired impact angle and impact time with look angle and lateral acceleration constraints.
31 sty 2022 · A moving virtual target that satisfies both impact time and angle requirements is introduced, which substantially simplifies the problem without estimating the time-to-go and its feasibility has been theoretically proved in this paper.
1 sty 2023 · This paper investigates the impact time and angle guidance problem against a non-maneuvering target in the 3D space. To address this challenging problem, an analytical 3D vector guidance law is developed by the command augmentation on an impact angle constrained guidance law with an explicit time-to-go estimation.
24 lut 2019 · For missile 1, it is obviously reasonable to choose a final time of 37.98 s, and for missiles 2, 3, and 4, 37.98 s is a larger final time, which is also reasonable. In conclusion, it is feasible to select the maximum impact time as the final impact time of all missiles.
1 mar 2019 · A novel cruise guidance method that can meet the terminal latitude and longitude, time and angle constraints independent of time-to-go prediction is studied in this paper. The impact time and angle control guidance (ITACG) goal is achieved through two steps.
26 wrz 2022 · [29] Hu Q., Cao R., Han T. and Xin M., “ Field-of-View Limited Guidance with Impact Angle Constraint and Feasibility Analysis,” Aerospace Science and Technology, Vol. 114, July 2021, Paper 106753.
