Suboptimal reentry guidance of a reusable launch vehicle using pitch plane maneuver

Aerospace Science and Technology

Volumn 14, Issue 6, 2010, Pages 377-386

  Chawla, C ^a   Sarmah, P ^a   Padhi, R ^a  

^a INDIAN INSTITUTE OF SCIENCE   (India)

Author keywords

Model predictive static programming; Reentry guidance; Reusable launch vehicle

Indexed keywords

COMPUTATIONALLY EFFICIENT; DEVELOPED MODEL; INITIAL CONDITIONS; MISSION PLANNING; REENTRY GUIDANCE; REUSABLE LAUNCH VEHICLES; STATIC PROGRAMMING; TERMINAL CONSTRAINT; TRAJECTORY OPTIMIZATION; VEHICLE LOAD;

AERODYNAMICS; LAUNCH VEHICLES; PLANNING; REUSABILITY; REUSABLE ROCKETS; VEHICLES;

LAUNCHING;

EID: 77956618544     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2010.04.001     Document Type: Article

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