Spacecraft Rendezvous Using Constant-Magnitude Low Thrust

Pini Gurfil

doi:10.2514/1.G007472

Spacecraft Rendezvous Using Constant-Magnitude Low Thrust

Pini Gurfil

Aerospace Engineering

Technion - Israel Institute of Technology

Research output: Contribution to journal › Comment/debate

Original language	English
Pages (from-to)	2183-2191
Number of pages	9
Journal	Journal of Guidance, Control, and Dynamics
Volume	46
Issue number	11
DOIs	https://doi.org/10.2514/1.G007472
State	Published - 2023

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

Keywords

Electric Propulsion
Feedback Control
Microsatellite
Orbital Maneuvers
Pontryagin's Minimum Principle
Space Exploration and Technology
Spacecraft Rendezvous

All Science Journal Classification (ASJC) codes

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

Access to Document

10.2514/1.G007472

Cite this

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title = "Spacecraft Rendezvous Using Constant-Magnitude Low Thrust",

keywords = "Electric Propulsion, Feedback Control, Microsatellite, Orbital Maneuvers, Pontryagin's Minimum Principle, Space Exploration and Technology, Spacecraft Rendezvous",

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year = "2023",

doi = "10.2514/1.G007472",

language = "الإنجليزيّة",

volume = "46",

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journal = "Journal of Guidance, Control, and Dynamics",

issn = "0731-5090",

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TY - JOUR

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AU - Gurfil, Pini

PY - 2023

Y1 - 2023

KW - Electric Propulsion

KW - Feedback Control

KW - Microsatellite

KW - Orbital Maneuvers

KW - Pontryagin's Minimum Principle

KW - Space Exploration and Technology

KW - Spacecraft Rendezvous

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M3 - تعليقَ / نقاش

SN - 0731-5090

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EP - 2191

JO - Journal of Guidance, Control, and Dynamics

JF - Journal of Guidance, Control, and Dynamics

IS - 11

ER -

Spacecraft Rendezvous Using Constant-Magnitude Low Thrust

UN SDGs

Keywords

All Science Journal Classification (ASJC) codes

Access to Document

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Cite this