In this chapter the optimization of low-energy transfers is treated. The concepts of trajectory optimization are recalled, and the direct transcription strategy is briefly sketched. The restricted three- and four-body problems are described, and their properties are discussed. Two different types of low-energy transfers are optimized: impulsive Earth–Moon exterior low-energy transfers and low-energy, low-thrust transfers to the L 1 periodic orbits of the Earth–Moon system.

Optimization of Low-Energy Transfers

TOPPUTO, FRANCESCO;
2013-01-01

Abstract

In this chapter the optimization of low-energy transfers is treated. The concepts of trajectory optimization are recalled, and the direct transcription strategy is briefly sketched. The restricted three- and four-body problems are described, and their properties are discussed. Two different types of low-energy transfers are optimized: impulsive Earth–Moon exterior low-energy transfers and low-energy, low-thrust transfers to the L 1 periodic orbits of the Earth–Moon system.
2013
Modeling and Optimization in Space Engineering
9781461444688
9781461444695
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/690687
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