Optimal field-of-view and impact-angle constrained guidance against a maneuvering target

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Authors: Tao Song, Yijing Wang, Hong Tao, Zeliang Wu
Cited by: 1
References: 33

Fields of Study & Subjects

Guidance and Control Systems Spacecraft Dynamics and Control Aerospace Engineering and Control Systems

Publication details

Journal / source
Aerospace Science and Technology
Publisher
Elsevier BV
Volume
179
Pages
113238–113238
Publication date
21 July 2026
Language
EN