Mstp Workshop 1996 -reentry Aerothermodynamics and Ground-to-flight Extrapolation Contributions to Hyperboloid Flare Test-cases I.c and Iii.b
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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, simultanceously. To meet this requirment a guidance law based on the fuzzy logic approach is developed. It is partitioned into three stages. This guidance law does not require linearization of missile engagement model. Line-of-sight and flight path ...
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تاریخ انتشار 2007