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Volumn , Issue , 1995, Pages 1046-1053

Guidance algorithm for suborbital flight experiment of unmanned lifting entry vehicle

Author keywords

[No Author keywords available]

Indexed keywords

DRAG; ORBITS; SPACE SHUTTLES;

EID: 84959097129     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1995-3286     Document Type: Conference Paper
Times cited : (1)

References (13)
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    • Davis, W.N.1
  • 2
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    • Nomura, S., Nakatani, I., and Ito, T., “Space Technologies Advance in Japan,” Aerospace America, Vol. 32, No. 2, February 1994, pp. 36-39.
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    • Nomura, S.1    Nakatani, I.2    Ito, T.3
  • 4
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    • Space Shuttle Entry Guidance Performance Results
    • November-December
    • Harpold, J. C. and Gavert, D. E., “Space Shuttle Entry Guidance Performance Results,” Journal of Guidance, Control, and Dynamics, Vol. 6, No. 6, November-December 1983, pp. 442-447.
    • (1983) Journal of Guidance, Control, and Dynamics , vol.6 , Issue.6 , pp. 442-447
    • Harpold, J.C.1    Gavert, D.E.2
  • 5
    • 0021973254 scopus 로고
    • Descent Guidance and Mission Planning for Space Shuttle
    • June
    • Joosten, B. K., “Descent Guidance and Mission Planning for Space Shuttle,” NASA CP-2342 Part 1, June 1983, pp. 113-124.
    • (1983) NASA CP , vol.2342 , pp. 113-124
    • Joosten, B.K.1
  • 6
    • 34249338498 scopus 로고
    • Re-entry Guidance through Closed-Form Equations
    • June
    • Tannas, L. E., Jr., “Re-entry Guidance through Closed-Form Equations,” AIAA Journal, Vol. 5, No. 6, June 1967, pp. 1102-1109.
    • (1967) AIAA Journal , vol.5 , Issue.6 , pp. 1102-1109
    • Tannas, L.E.1
  • 8
    • 0028550587 scopus 로고
    • Shuttle Entry Guidance Revisited Using Nonlinear Geometric Methods
    • November-December
    • Mease, K. D. and Kremer, J.-P., “Shuttle Entry Guidance Revisited Using Nonlinear Geometric Methods,” Journal of Guidance, Control, and Dynamics, Vol. 17, No. 6, November-December 1994, pp. 1350-1356.
    • (1994) Journal of Guidance, Control, and Dynamics , vol.17 , Issue.6 , pp. 1350-1356
    • Mease, K.D.1    Kremer, J.-P.2
  • 9
    • 0024051348 scopus 로고
    • Flight Control Design Using Non-linear Inverse Dynamics
    • Lane, S. H. and Stengel, R. F., “Flight Control Design Using Non-linear Inverse Dynamics,” Automatica, Vol. 24, No. 4, 1988, pp. 471-483.
    • (1988) Automatica , vol.24 , Issue.4 , pp. 471-483
    • Lane, S.H.1    Stengel, R.F.2
  • 10
    • 0026897323 scopus 로고
    • Approach Guidance in a Downburst
    • July-August
    • Zhao, Y. and Bryson, A. E., “Approach Guidance in a Downburst,” Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, July-August 1992, pp. 893-900.
    • (1992) Journal of Guidance, Control, and Dynamics , vol.15 , Issue.4 , pp. 893-900
    • Zhao, Y.1    Bryson, A.E.2
  • 11
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    • Addendum to 'Heat Transfer to Satellite Vehicles Reentering the Atmosphere
    • December
    • Detra, R. W., Kemp, N. H., and Riddell, F. R., “Addendum to 'Heat Transfer to Satellite Vehicles Reentering the Atmosphere',” Jet Propulsion, Vol. 27, December 1957, pp. 1256-1257.
    • (1957) Jet Propulsion , vol.27 , pp. 1256-1257
    • Detra, R.W.1    Kemp, N.H.2    Riddell, F.R.3
  • 13
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    • National Oceanic and Atmospheric Administration, NASA, and U S. Air Force, Washington, D.C., October
    • U.S. Standard Atmosphere, 1976, National Oceanic and Atmospheric Administration, NASA, and U S. Air Force, Washington, D.C., October 1976.
    • (1976)


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.