Robustness analysis of an adaptive re-entry guidance system

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

Volumn 4, Issue , 2005, Pages 2941-2951

  Mooij, E ^a,b,c  

^a AIRBUS DEFENCE AND SPACE   (Germany)

^b Advanced Systems and Engineering Division   (Netherlands)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN PARAMETERS; FEEDBACK CONTROLLER; OPERATING CONDITIONS; RE-ENTRY VEHICLE; SIMPLE ADAPTIVE CONTROL THEORY; TRACKING;

ADAPTIVE CONTROL SYSTEMS; FLIGHT SIMULATORS; MONTE CARLO METHODS; OPTIMIZATION; PARAMETER ESTIMATION; REENTRY; ROBUSTNESS (CONTROL SYSTEMS); STRUCTURAL DESIGN; TRAJECTORIES;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 29744446514     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Kaufman, H., Barkana, I. and Sobel, K., Direct adaptive control algorithms: Theory and applications, Second edition, Springer-Verlag, New York, 1998.
2. Mooij, E., "Model Reference Adaptive Guidance for Re-entry Trajectory Tracking ", AIAA-04-4775, From: AIAA Guidance, Navigation, and Control Conference, Piovidence, RI, August l6-19, 2004a.
3. MBB Space Communication and Propulsion Systems-Division, "Study on re-entry guidance and control", ESA report reference: ESA CR (P) 2652, Munich, 1988.
4. Mooij, E., "Aerospace-plane flight dynamics: analysis of guidance and control concepts", PhD thesis, Delft University of Technology, Faculty of Aerospace Engineering, 1998.
5. Mooij, E., "Evolutionary Optimisation of a Model Reference Adaptive Control System", AIAA-02-4922, From: AIAA Guidance, Navigation, and Control Conference, Monterey, CA, August 6-9, 2002.