Robust Optimisation of Trajectories Intercepting Dangerous NEO-Reference-Cited by-同舟云学术

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Robust Optimisation of Trajectories Intercepting Dangerous NEO

Published:2002-06-25 Issue: Volume: Page:
ISSN:
Container-title:AIAA/AAS Astrodynamics Specialist Conference and Exhibit
language:
Short-container-title:

Author:

Vasile Massimiliano¹

Affiliation:

1. European Space Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-4719

Reference7 articles.

1. Accettura A.G.,Bruno C,Marzari F.,Casotto S.Mission to Mars Using Integrated Propulsion Concepts:Considerations,Opportunities and Strategies. IAF-01-R.4.08,IAF 2001,October 1-5, Toulouse, France

2. Vasile M. Direct Transcription by FET for Optimal Space Trajectory Design. Internal Report DIA-SR 99-02, Politecnico di Milano, Dipartimento di Ingegneria Aerospaziale, March1999.

3. Multicriteria Design Optimization

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