Near time-optimal feedback instantaneous impact point (IIP) guidance law for rocket
نویسندگان
چکیده
منابع مشابه
Guidance Law for Impact Time Control
A nonlinear guidance law is presented for the im-pact time control of an interceptor against a stationary target. Exact closed form expressions for impact time and the guidance command are derived. For a given engagement geometry, a given impact time corresponds to a unique initial heading error. For interceptors launched with any other initial heading error, a term proportional to impact time ...
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ژورنال
عنوان ژورنال: Aerospace Science and Technology
سال: 2018
ISSN: 1270-9638
DOI: 10.1016/j.ast.2018.02.024