Energy Optimal Midcourse Guidance Law Design Based on Predicted Interception Point

Sie sind hier: Homepage > Suche

Energy Optimal Midcourse Guidance Law Design Based on Predicted Interception Point

Fang, Yi / Ludan, Li / Yaosheng, Hu

Aiming at the interception problem of the hypersonic aircraft during its coast phase, the Singer Model was used to perform target trajectory prediction based on the early-warning information, and the predicted interception point between the interceptor and the hypersonic target was calculated accordingly. An energy optimal guidance law based on the predicted interception point was designed for the midcourse of the interceptor, and the Uncertain Interval was considered for the existence of various errors to avoid control effort’s oscillations around zero. Simulation experiments are conducted to illustrate the performance of the proposed method.

Zugriff

Zugriff prüfen

Verfügbarkeit in meiner Bibliothek prüfen

Bestellung bei Subito €

Exportieren, teilen und zitieren

Dokumentinformationen

Titel :

Energy Optimal Midcourse Guidance Law Design Based on Predicted Interception Point

Weitere Titelangaben:

Lect. Notes Electrical Eng.

Beteiligte:

Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Yu, Xiang (Herausgeber:in) / Fang, Yi (Autor:in) / Ludan, Li (Autor:in) / Yaosheng, Hu (Autor:in)

Erschienen in:

Advances in Guidance, Navigation and Control ; Kapitel : 372 ; 4483-4496

Lecture Notes in Electrical Engineering ; 644

Erscheinungsdatum :

2021-10-30

Format / Umfang :

14 pages

ISBN :

978-981-15-8155-7 , 978-981-15-8154-0

ISSN :

1876-1119 , 1876-1100

DOI :