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Volumn 7, Issue 3, 1999, Pages 295-303

Fuzzy guidance of the shuttle orbiter during atmospheric reentry

Author keywords

Approximations; Fuzzy inference; Guidance laws; Shuttle reentry; Surface tracking

Indexed keywords

COMPUTER SIMULATION; ELECTRONIC GUIDANCE SYSTEMS; INFERENCE ENGINES; SPACE SHUTTLES;

EID: 0033100465     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(98)00188-9     Document Type: Article
Times cited : (2)

References (17)
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  • 2
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    • 16-19 February 1997, Albuquerque, New Mexico
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  • 3
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    • 21 January
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    • Harpold, J.1
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  • 6
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    • Homaifar, A.1    Clifton, C.2    Bikdash, M.3
  • 7
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    • Shuttle entry guidance revisited using nonlinear geometric methods
    • Mease, K., & Kremer, J. (1994). Shuttle entry guidance revisited using nonlinear geometric methods. J. Guidance Control Dyn. 17(6), 1350-1356.
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    • Mease, K.1    Kremer, J.2
  • 9
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    • Training Manual
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  • 12
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    • Re-entry control to a drag-vs-energy profile
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  • 16
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.