Multi-Phase Trajectory Optimisation for Access-to-Space with RBCC-Powered TSTO via Surrogated-Assisted Hybrid Evolutionary Algorithms Incorporating Pseudo-Spectral Methods-Reference-Cited by-同舟云学术

Multi-Phase Trajectory Optimisation for Access-to-Space with RBCC-Powered TSTO via Surrogated-Assisted Hybrid Evolutionary Algorithms Incorporating Pseudo-Spectral Methods

Published:2014-06-13 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
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Author:

Ogawa Hideaki¹,Kodera Masatoshi²,Tomioka Sadatake²,Ueda Shuichi²

Affiliation:

1. RMIT University

2. Japan Aerospace Exploration Agency (JAXA)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2360

Reference18 articles.

1. Conceptual Study of a Rocket-Ramjet Combined-Cycle Engine for an Aerospace Plane

2. Multi-Objective Design and Trajectory Optimization of Space Transport Systems with RBCC Propulsion via Evolutionary Algorithms and Pseudospectral Methods

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