Quadratic-Based Computation of Four-Impulse Optimal Rendezvous near Circular Orbit

By T. Carter, Sergio A. Alvarez. 2000

63 citations recorded by the source corpus.

Subfields: Aerospace Engineering

View Paper: https://www.semanticscholar.org/paper/13e55c0f69234c0e91ae93667057229f302be4b4

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In Aerospace Engineering

1. G. Tang
2. Ya-zhong Luo

Citations in the corpus

• Optimal Multi-Objective Linearized Impulsive Rendezvous (2007, background): “Introduction T HE optimal multiple-impulse spacecraft rendezvous problem has been studied extensively by a number of groups, such as Prussing [1,2], Gross and Prussing [3], Jones , and Prussing andChiu [5], and recently by Shen and Tsiotras [6], Kim and Spencer [7], Prussing [8], Carter and Brient [”