Paper Title :Guidance Law For Impact Time Control
Author :Abdul Saleem, Ashwini Ratnoo
Article Citation :Abdul Saleem ,Ashwini Ratnoo ,
(2015 ) " Guidance Law For Impact Time Control " ,
International Journal of Electrical, Electronics and Data Communication (IJEEDC) ,
pp. 11-14,
Volume-3, Issue-7
Abstract : 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 error is augmented with the guidance command. The control parameter of the
guidance command is adjusted in a feedback form so that the proposed method is robust to autopilot dynamics. The method
is used in salvo attack, where multiple interceptors are launched for a simultaneous impact.
Type : Research paper
Published : Volume-3, Issue-7
DOI - 10.18479/ijeedc/2015/v3i7/48252
Copyright: © Institute of Research and Journals
|
 |
| |
 |
PDF |
| |
Viewed - 109 |
| |
Published on 2015-07-04 |
|