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Volumn 12, Issue 3, 2004, Pages 291-298

Design of generalized conceptual guidance law using aim angle

Author keywords

Aim angle; Autopilot dynamics; Collision triangle; Conceptual guidance law; Lyapunov approach

Indexed keywords

DESIGN; ERROR ANALYSIS; MISSILES;

EID: 1142305274     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(03)00097-2     Document Type: Article
Times cited : (29)

References (15)
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  • 2
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    • Dayton, OH, USA
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  • 3
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    • Ben-Asher, J.Z.1    Yaesh, I.2
  • 4
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    • Implementation of optimal guidance laws using predicted missile velocity profiles
    • Cho, H., Ryoo, C., & Tahk, M. (1999). Implementation of optimal guidance laws using predicted missile velocity profiles. Journal of Guidance, Control, and Dynamics, 22(4), 579-588.
    • (1999) Journal of Guidance, Control, and Dynamics , vol.22 , Issue.4 , pp. 579-588
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  • 6
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    • Moon, J.1    Kim, K.2    Kim, Y.3
  • 11
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    • Fuzzy logic implementation of proportional navigation guidance
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  • 12
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    • A Lyapunov-like approach to performance analysis of 3-dimensional pure PNG laws
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.