Impact of non-latching booms on a nanosatellite attitude control system

Author:

Quevedo Mantovani LorenzzoORCID,Gomes dos Santos WillerORCID,Cardoso-Ribeiro Flávio LuizORCID,Vergueiro Loures da Costa Luis Eduardo

Funder

Fundação de Amparo à Pesquisa do Estado de São Paulo

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference45 articles.

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3. Attitude determination strategy based on Kalman filter for the sport cubesat science mission;Santos;Adv. Astronaut. Sci.,2020

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5. Conceptual design and finite element method validation of a new type of self-locking hinge for deployable CubeSat solar panels;Solís-Santomé;Adv. Mech. Eng.,2019

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Attitude Determination and Control in Small Satellites: A Review;IEEE Journal on Miniaturization for Air and Space Systems;2024-09

2. Influence of thrust modulation on a satellite with flexible non-latching booms;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2022-11-16

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