Spacecraft design optimization is a domian that can benefit from the application of optimization algorithms such as genetic algorithms. In this paper, we describe DEVO, an evolutionary optimization system that addresses these issues and provides a tool that can be applied to a number of real-world spacecraft design applications. We describe two current applications of DEVO: physical design if a Mars Microprobe Soil Penetrator, and system configuration optimization for a Neptune Orbiter.
An Evolutionary Optimization System for Spacecraft Design
1997-06-10
Preprint
No indication
English
13.0403 Evolutionary Computing for Spacecraft Power Subsystem Design Search and Optimization
British Library Conference Proceedings | 2004
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