Atmospheric ascent guidance for rocket-powered launch vehicles

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Dukeman, Greg A ^a  

^a NASA MARSHALL SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY VALUE PROBLEMS; CALCULATIONS; LAUNCH VEHICLES; TRAJECTORIES;

ATMOSPHERIC EFFECTS; CALCULUS OF VARIATIONS; CUT-OFF CONDITIONS; HIGH DYNAMIC PRESSURE; LAUNCH VEHICLE TRAJECTORY; MULTIPLE SHOOTING; NUMERICAL TECHNIQUES; TWO POINT BOUNDARY VALUE PROBLEMS;

ROCKETS;

EID: 85085779483     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4559     Document Type: Conference Paper

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