DocumentCode :
2716379
Title :
Bio-inspired computing for launch vehicle design and trajectory optimization
Author :
Suresh, Sundaram ; Rong, Hai-Jun ; Sundararajan, Narasimhan
Author_Institution :
Dept. of Electr. Eng., Indian Inst. of Technol., Delhi, India
fYear :
2009
fDate :
8-10 July 2009
Firstpage :
1
Lastpage :
8
Abstract :
This paper presents an optimization tool for launch vehicle design and trajectory optimization using bio-inspired computing algorithms and nonlinear programming. The objective is to size a launch vehicle such that the payload to lift-of-weight ratio is maximized (i.e the lift off weight is a minimum). Here, the staging problem is solved using Particle Swarm Optimization (PSO) method. With the above vehicle, an optimal trajectory is arrived at using a Real-Coded Genetic Algorithm (RCGA) and solving a nonlinear programming (NLP) by the direct shooting method. The solutions from PSO and RCGA are used for initialization of NLP variables. A case study is carried out that establishes the advantage of the proposed approach.
Keywords :
aircraft; genetic algorithms; nonlinear programming; particle swarm optimisation; position control; bio-inspired computing; launch vehicle design; nonlinear programming; particle swarm optimization; real-coded genetic algorithm; trajectory optimization; Algorithm design and analysis; Design optimization; Engines; Genetic algorithms; Orbits; Particle swarm optimization; Propulsion; Rockets; Satellites; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computational Intelligence for Security and Defense Applications, 2009. CISDA 2009. IEEE Symposium on
Conference_Location :
Ottawa, ON
Print_ISBN :
978-1-4244-3763-4
Electronic_ISBN :
978-1-4244-3764-1
Type :
conf
DOI :
10.1109/CISDA.2009.5356548
Filename :
5356548
Link To Document :
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