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Volumn 10, Issue 3, 2006, Pages 222-232

Overview of some optimal control methods adapted to expendable and reusable launch vehicle trajectories

Author keywords

Launcher; Optimization; Trajectory

Indexed keywords

OPTIMIZATION; PROBLEM SOLVING; SPACE FLIGHT; TRAJECTORIES;

EID: 33646469132     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2005.11.004     Document Type: Article
Times cited : (28)

References (6)
  • 1
    • 33646492371 scopus 로고    scopus 로고
    • C. Aumasson, Ph. Landiech, Méthode Itérative de type Gradient Projeté Généralisé pour l'Optimisation Paramétrique et Fonctionnelle de Systèmes Dynamiques soumis à des Contraintes, ONERA NT 1988-9
  • 2
    • 0032021498 scopus 로고    scopus 로고
    • Survey of numerical methods for trajectory optimization
    • Betts J.T. Survey of numerical methods for trajectory optimization. J. Guidance Control Dynam. 21 2 (1998)
    • (1998) J. Guidance Control Dynam. , vol.21 , Issue.2
    • Betts, J.T.1
  • 3
    • 33646480973 scopus 로고    scopus 로고
    • D. Iranzo-Greuz, F. Deneu, M. Malassigné, N. Bérend, C. Jolly, Preliminary scenarios for the return to the launch site of the first stage of a TSTO RLV, in: AAAF 3rd International Symposium on Atmospheric Reentry Vehicles and Systems, Arcachon, France, 24-27 March 2003
  • 4
    • 84896848093 scopus 로고    scopus 로고
    • C. Jolly, N. Bérend, C. Aumasson, FLOP: ONERA's answer to trajectory optimization for future launchers, in: AIAA Flight Mechanics Conference, Austin, USA, 11-14 August 2003


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.