General Perturbation Method for Satellite Constellation Deployment Using Nodal Precession-Reference-Cited by-同舟云学术

General Perturbation Method for Satellite Constellation Deployment Using Nodal Precession

Published:2020-04 Issue:4 Volume:43 Page:814-824
ISSN:1533-3884
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

McGrath Ciara N.¹,Macdonald Malcolm¹

Affiliation:

1. University of Strathclyde, Glasgow, Scotland G1 1XJ, United Kingdom

Funder

Engineering and Physical Sciences Research Council

Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.G004443

Reference21 articles.

1. LalB.de la Rosa BlancoE.BehrensJ. R.CorbinB. A.GreenE. K.PicardA. J.BalakrishnanA. “Global Trends in Small Satellites,” IDA Science and Technology Policy Inst., IDA Paper P-8638, July 2017.

2. Survey of worldwide pico- and nanosatellite missions, distributions and subsystem technology

3. Status and Trends of Smallsats and their Launch Vehicles — An Up-to-date Review

4. Launch and deployment of distributed small satellite systems

5. Mission Results from FORMOSAT-3/COSMIC Constellation System

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