Constraint Handling and Multi-Objective Methods for the Evolution of Interplanetary Trajectories

Author:

Izzo Dario1,Hennes Daniel1,Riccardi Annalisa1

Affiliation:

1. European Space Research and Technology Centre, ESA, 2201 AZ Noordwijk, The Netherlands

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference30 articles.

1. MinovitchM. “Alternative Method for Determination of Elliptic and Hyperbolic Trajectories,” NASA TM-312-118, Feb. 1961.

2. MinovitchM. “Method for Determining Interplanetary Free-Fall Reconnaissance Trajectories,” NASA TM-312-130, Feb. 1961.

3. Near-optimal low-thrust orbit transfers generated by a genetic algorithm

4. Near-Optimal Low-Thrust Trajectories via Micro-Genetic Algorithms

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