A Three Stage Terminal Fuzzy Guidance Law for Reentry Vehicles

An advanced guidance law is developed for reentry phase of a reentry vehicle. it can achieve small miss distance and desired impact attitude angle, simultaneously. to meet this requirement, a guidance law based on the fuzzy logic control approach is developed. it is partitioned into three stages. this guidance law does not require linearization of missile engagement model. line-of-sight angle and flight path angle are used to constitute the rule antecedent of the guidance law to shape an appropriate flight trajectory for engagement. numerical simulation results and comparison with an existing algorithm demonstrated that the proposed guidance law offers satisfactory performance and robustness, fulfilling its design goals.