Multi-Objective Low-Thrust Trajectory Optimisation: Variable and Constant Specific Impulse

Details Multi-Objective Low-Thrust Trajectory Optimisation: Variable and Constant Specific Impulse Multi-Objective Low-Thrust Trajectory Optimisation: Variable and Constant Specific Impulse

Oct 2004

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004esasp.555e..83p&link_type=abstract

Proceedings of the 4th International Spacecraft Propulsion Conference (ESA SP-555). 2-9 June, 2004, Chia Laguna (Cagliari), Sard

Computer Science

Performance

Scientific paper

Variable and constant specific impulse electric propulsion are compared by evaluating their performance by means of the 2-D trajectory optimisation of different missions. The main purpose of this paper is to evaluate the advantage given by variable specific impulse in comparison with constant specific impulse. The optimisation was performed by using multi-objective evolutionary algorithms. Pareto fronts comparing time of flight and useful mass are used to analyse the mission results through the two conflicting objectives.

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