Control laws for minimum orbital change-the satellite retrieval problem

T. Cichan; R. G. Melton; D. B. Spencer

doi:10.2514/2.4842

Control laws for minimum orbital change-the satellite retrieval problem

T. Cichan, R. G. Melton, D. B. Spencer

Research output: Contribution to journal › Article › peer-review

1 Scopus citations

Abstract

Satellite retrieval might require expending unused propellant for safety reasons prior to the retrieval. Blended extremal controls that minimize changes in semimajor axis, eccentricity, and inclination during a single, constant-thrust burn can result in modest requirements for thrust seeing. The method is shown to produce acceptable changes in these orbital elements. The optimization program finds solutions that include very little out-of-plane thrusting.

Original language	English (US)
Pages (from-to)	1231-1233
Number of pages	3
Journal	Journal of Guidance, Control, and Dynamics
Volume	24
Issue number	6
DOIs	https://doi.org/10.2514/2.4842
State	Published - 2001

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Applied Mathematics
Electrical and Electronic Engineering
Control and Systems Engineering
Space and Planetary Science

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10.2514/2.4842

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title = "Control laws for minimum orbital change-the satellite retrieval problem",

abstract = "Satellite retrieval might require expending unused propellant for safety reasons prior to the retrieval. Blended extremal controls that minimize changes in semimajor axis, eccentricity, and inclination during a single, constant-thrust burn can result in modest requirements for thrust seeing. The method is shown to produce acceptable changes in these orbital elements. The optimization program finds solutions that include very little out-of-plane thrusting.",

author = "T. Cichan and Melton, {R. G.} and Spencer, {D. B.}",

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AU - Melton, R. G.

AU - Spencer, D. B.

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AB - Satellite retrieval might require expending unused propellant for safety reasons prior to the retrieval. Blended extremal controls that minimize changes in semimajor axis, eccentricity, and inclination during a single, constant-thrust burn can result in modest requirements for thrust seeing. The method is shown to produce acceptable changes in these orbital elements. The optimization program finds solutions that include very little out-of-plane thrusting.

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JO - Journal of Guidance, Control, and Dynamics

JF - Journal of Guidance, Control, and Dynamics

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ER -

Control laws for minimum orbital change-the satellite retrieval problem

Abstract

All Science Journal Classification (ASJC) codes

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