메뉴 건너뛰기




Volumn 1017, Issue , 2004, Pages 210-233

Finite burn maneuver modeling for a generalized spacecraft trajectory design and optimization system

Author keywords

Primer vector theory; Spacecraft trajectory design; Spacecraft trajectory optimization; Trajectory optimization

Indexed keywords

CONFERENCE PAPER; EXPERIMENTAL MODEL; GRAVITY; MASS; MATHEMATICAL COMPUTING; SPACE FLIGHT; THEORETICAL STUDY; TIME; UNITED STATES; VELOCITY;

EID: 3042833856     PISSN: 00778923     EISSN: None     Source Type: Book Series    
DOI: 10.1196/annals.1311.013     Document Type: Conference Paper
Times cited : (41)

References (16)
  • 6
    • 0344252560 scopus 로고
    • Primer Vector Theory and Applications
    • NASA Johnson Space-flight Center, Houston, Texas
    • JEZEWSKI, D.J. 1975. Primer Vector Theory and Applications. NASA Technical Report R-454, NASA Johnson Space-flight Center, Houston, Texas.
    • (1975) NASA Technical Report R-454
    • Jezewski, D.J.1
  • 14
    • 84989068908 scopus 로고
    • Adjoint control transformations for solving practical optimal control problems
    • Wiley Interscience
    • DIXON, L.C. & M.C. BARTHOLOMEW-BIGGS. 1981. Adjoint control transformations for solving practical optimal control problems. In Optimal Control Applications and Methods, Vol. 2. Wiley Interscience.
    • (1981) Optimal Control Applications and Methods , vol.2
    • Dixon, L.C.1    Bartholomew-Biggs, M.C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.