Hybrid entry guidance for reusable launch vehicles

Yuhang Xuebao/Journal of Astronautics

Volumn 28, Issue 1, 2007, Pages 213-217

  Hu, Jian Xue ^a   Chen, Ke Jun ^a   Zhao, Han Yuan ^a   Yu, Meng Lun ^b  

^a NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY   (China)

^b CHINA ACADEMY OF LAUNCH VEHICLE TECHNOLOGY   (China)

Author keywords

Dispersion analysis; Entry guidance; Online entry trajectory generation; Predictor corrector guidance; Reusable launch vehicle

Indexed keywords

COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); NAVIGATION; SPACE FLIGHT;

DISPERSION ANALYSIS; ENTRY GUIDANCE; ONLINE ENTRY TRAJECTORY GENERATION; PREDICTOR CORRECTOR GUIDANCE; REUSABLE LAUNCH VEHICLE;

REENTRY;

EID: 34248328805     PISSN: 10001328     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (11)

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