An Optimized Plane-Change Solution for Microsatellite Formation Flying-Reference-Cited by-同舟云学术

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An Optimized Plane-Change Solution for Microsatellite Formation Flying

Published:2022-12 Issue:4 Volume:3 Page:211-220
ISSN:2576-3164
Container-title:IEEE Journal on Miniaturization for Air and Space Systems
language:
Short-container-title:IEEE J. Miniat. Air Space Syst.

Author:

Goh Shu Ting¹^ORCID,Low Samuel Y. W.²^ORCID,Low Kay-Soon¹^ORCID,Poh Eng Kee³

Affiliation:

1. Satellite Technology and Research Centre, National University of Singapore, Queenstown, Singapore

2. Aeronautics and Astronautics Department, Stanford University, Stanford, CA, USA

3. School of Electrical and Electronics Engineering, Nanyang Technological University, Jurong West, Singapore

Funder

National Research Foundation (NRF) Singapore, Office for Space Technology and Industry (OSTin) through the NUS Formation Flying Microsatellites Program

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Pharmacology (medical)

Link

http://xplorestaging.ieee.org/ielx7/8253411/9961123/09899487.pdf?arnumber=9899487

Reference43 articles.

1. Implementation of Interior-Point Methods for Large Scale Linear Programs

2. Constraint Estimation of Spacecraft Positions

3. Spacecraft propulsion, launch systems, and launch mechanics;pisacane;Fundamentals of Space Systems,2005

4. The formulation and testing of new solid propellant mixture (DB+x%BP) for a new MEMS-based microthruster

5. An inequality constrained ensemble Kalman Filter for parameter estimation application

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