Optimal Guidance Law for Critical Safe Miss Distance Evasion
In pursuit–evasion scenarios, the pursuer typically possesses a lethal zone. If the evader effectively utilizes perceptual information, they can narrowly escape the lethal zone while minimizing energy consumption, thereby avoiding excessive and unnecessary maneuvers. Based on optimal control theory, we propose a guidance law for achieving critical safe miss distance evasion under bounded control. First, we establish the zero-effort miss (ZEM) state equation for the evader, while approximating disturbances from the pursuer. Next, we formulate an optimal control problem with energy consumption as the objective function and the ZEM at the terminal time as the terminal constraint. Subsequently, we design an iterative algorithm that combines the homotopy method and Newton’s iteration to solve the optimal control problem, applying Pontryagin’s Maximum Principle. The simulation results indicate that the designed iterative method converges effectively; through online updates, the proposed guidance law can successfully achieve critical safe miss distance evasion. Compared to programmatic maneuvering and norm differential game guidance law, this approach not only stabilizes the evader’s evasion capabilities but also significantly reduces energy consumption.
Authors
- C Wang
- Yang Chen (ORCID: https://orcid.org/0000-0002-5723-4743)
- Rui Lyu
- Zhuo Liang (ORCID: https://orcid.org/0000-0002-4700-4207)
- J.L. Yan
Institutions
- China Academy of Launch Vehicle Technology (CN)
Publication Details
- Journal
- Aerospace
- Published
- 2024-12-19
- DOI
- https://doi.org/10.3390/aerospace11121041
- Citations
- 2
- Primary Topic
- Guidance and Control Systems
- Type
- article
- Field-Weighted Citation Impact
- 2.60