Reentry Trajectory optimization: Evolutionary approach

9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization

Volumn , Issue , 2002, Pages

  Arora, Rajesh Kumar ^a  

^a INDIAN SPACE RESEARCH ORGANISATION   (India)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; EQUATIONS OF MOTION; HEAT FLUX; OPTIMIZATION; REENTRY; REUSABILITY; SPACE SHUTTLES;

CONVENTIONAL METHODS; COSTATE EQUATIONS; DYNAMIC PRESSURES; EVOLUTIONARY APPROACH; REENTRY TRAJECTORY OPTIMIZATIONS; REUSABLE LAUNCH VEHICLES; STANDARD OPTIMIZATION METHOD;

GENETIC ALGORITHMS;

EID: 79960982832     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. ED Dickmans, "Maximum range 3D lifting planetary entry", NASA TR R-387
2. Timothy E McQuade, "Trajectory optimization in the presence of constraints", MIT, 1989
3. Denhan, Walter F and Bryson, Auther E, "Optimal programming problems with inequality constraints II: solution by steepest ascent", AIAA Journal, 2, (1964),25-34
4. David E Goldberg, "Genetic algorithm in search, optimization and machine learning", Addison - Wessley
5. Lu Xuefu, Nan Ying, "The optimal return trajectory design of space vehicle", AAS 93-348
6. Zbigneiew Michalewicz, "Genetic algorithm + data structure = evolution program", Springer
7. Jean-Antoine Desidei, Sergey Peigen, Sergey Timchenko, "Application of genetic algorithm to space vehicle reentry trajectory optimization problem", INRI No. 3843, Dec.1999
8. Jon C Hapold, Claude A Graves Jr., "Shuttle Entry Guidance", Journal of Astronautical Science, Vol. XXVII, No.3, 1979, pp 239-268