Solving multi-objective aeroassisted spacecraft trajectory optimization problems using extended NSGA-II

Runqi Chai, Al Savvaris, Antonios Tsourdos, Senchun Chai

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

14 Citations (Scopus)

Abstract

This paper focuses on the application of an extended NSGA-II algorithm to the aeroassisted spacecraft trajectory optimization problems. A new multi-objective spacecraft optimal control model is formulated and parameterized using discretization method. The resulting multi-objective nonlinear programming problem is then solved via the multiobjective evolutionary solver. In order to deal with path constraints that naturally arise in practical trajectory planning problems, the original NSGA-II approach is extended by introducing a new constraint handling strategy. Simulation results are provided to illustrate the effectiveness and feasibility of the enhanced NSGA-II algorithm in dealing with spacecraft trajectory optimization problems.

Original languageEnglish
Title of host publicationAIAA SPACE and Astronautics Forum and Exposition
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624104831
DOIs
Publication statusPublished - 2017
EventAIAA Space and Astronautics Forum and Exposition, SPACE 2017 - Orlando, United States
Duration: 12 Sept 201714 Sept 2017

Publication series

NameAIAA SPACE and Astronautics Forum and Exposition, SPACE 2017
Volume0

Conference

ConferenceAIAA Space and Astronautics Forum and Exposition, SPACE 2017
Country/TerritoryUnited States
CityOrlando
Period12/09/1714/09/17

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