Fuzzy guidance of the shuttle orbiter during atmospheric reentry

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North Carolina A and T State Univ, Greensboro, United States ^{[1
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Control Eng Pract | / 3卷 / 295-303期

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[1] Fuzzy guidance of the shuttle orbiter during atmospheric reentry
Bikdash, M
Sartor, K
Homaifar, A
CONTROL ENGINEERING PRACTICE, 1999, 7 (03) : 295 - 303
[2] CHARACTERISTICS OF THE SHUTTLE ORBITER LEESIDE FLOW DURING A REENTRY CONDITION
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[3] SHUTTLE ORBITER REENTRY FLOWFIELDS AT HIGH ANGLE OF ATTACK
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[4] REENTRY CONTROL EFFECTIVENESS METHODOLOGY FOR SPACE-SHUTTLE-ORBITER
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JOURNAL OF SPACECRAFT AND ROCKETS, 1977, 14 (11) : 669 - 675
[5] IMPACT OF SPACE-SHUTTLE ORBITER REENTRY ON MESOSPHERIC NOX
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[6] Shuttle reentry guidance using Sugeno approximation
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[7] SHUTTLE ORBITER GUIDANCE SYSTEM FOR TERMINAL FLIGHT PHASE
EHLERS, HL
KRAEMER, JW
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[8] REENTRY CONTROL EFFECTIVENESS METHODOLOGY FOR SPACE-SHUTTLE ORBITER - COMMENT
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REDING, JP
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[9] SHUTTLE ORBITER - COMBINED SPACE ATMOSPHERIC VEHICLE PROGRESSES
不详
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[10] Efficient calculation method of subsonic aerodynamic characteristics for a space shuttle orbiter in the reentry attitude
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