Reentry guidance for generic RLV using optimal perturbations and error weights

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 8, Issue , 2005, Pages 5857-5870

  Joshi, Ashok ^a,b,c   Sivan, K ^a,b,c  

^a INDIAN INSTITUTE OF TECHNOLOGY BOMBAY   (India)

^b Department of Aerospace Engineering ^*  (India)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CONTROL SYSTEM ANALYSIS; ERROR ANALYSIS; LEARNING ALGORITHMS; OPTIMAL CONTROL SYSTEMS; PHASE EQUILIBRIA; TRAJECTORIES;

CONTROL VECTOR FORMULATION; ERROR WEIGHTS; OPTIMAL PERTURBATIONS; REUSABLE LAUNCH VEHICLES;

REENTRY;

EID: 29744452173     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-6438     Document Type: Conference Paper

References (9)

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3. Ishizuka, K, Shimura, K, and Ishimoto, S., "A Reentry Guidance Law Employing Simple Real-Time Integration", AIAA Paper No. AIAA-98-4329, 1998
4. Fuhry, D.P., "Adaptive Atmospheric Reentry Guidance for the Kistler K-I Orbital Vehicle", AIAA Paper No. AIAA-99-4211, 1999.
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6. Youssef, H., Chowdhary, R.S., Lee, H., Rodi, P., and Zimmermann, C., "Predictor-Corrector Entry Guidance for Reusable Launch Vehicles", AIAA Guidance, Navigation and Control Conference, 6-9, August 2001, AIAA Paper No. AIAA 2001-4043.
7. Sivan, K., Joshi, A. and Suresh, B. N., "Reentry Trajectory Modeling and Simulation: Application to Reusable Launch vehicle Mission", Proc. of International Conference on Modeling, Simulation, Optimization for Design of Multi-disciplinary Engineering System (MSO-DMES), Sept 24-26, 2003, Goa, India.
8. th International Symposium on Atmospheric Reentry Vehicle and Systems, March 21-23, 2005, Arcachon, France
9. Eussel, W.R.,(Ed.), "Aerodynamic Design Data Book, Volume-I, Orbiter Vehicle SIS-1", Report No. SD72-SH-0060, Space Systems Group, Rockwell International, California, 1980.