Guidance Law Design for Space-Based Anti-Missile Boost Phase Intercept
Guidance law The optimal direct-impact guidance law for space-based anti-missile of ballistic missile in boost phase is considered. First the relative motion equation between missile and target is built, then the optimal guidance law based on terminal miss distance is designed. using minimum energy as the optimum index. The simulation results show the effectiveness of our guidance law.
Riza Esa and Yanwen Wu
H. Huang and Z. F. Zhu, "Guidance Law Design for Space-Based Anti-Missile Boost Phase Intercept", Advanced Materials Research, Vols. 301-303, pp. 1749-1753, 2011