Efficient Fast Open-Loop Attitude Control Strategy for Earth Imaging Nanospacecraft-Reference-Cited by-同舟云学术

Efficient Fast Open-Loop Attitude Control Strategy for Earth Imaging Nanospacecraft

Published:2017-09 Issue:5 Volume:30 Page:04017057
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Grossi Armando¹,Piergentili Fabrizio²,Santoni Fabio³

Affiliation:

1. Graduate Student, Faculty of Civil and Industrial Engineering, Univ. of Rome “La Sapienza,” Via Eudossiana 18, 00184 Rome, Italy (corresponding author).

2. Assistant Professor, Dipartimento di Ingegneria Meccanica e Aerospaziale, Univ. of Rome “La Sapienza,” Via Eudossiana 18, 00184 Rome, Italy.

3. Associate Professor, Dipartimento di Ingegneria Astronautica, Elettrica ed Energetica, Univ. of Rome “La Sapienza,” Via Eudossiana 18, 00184 Rome, Italy.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000773

Reference15 articles.

1. New results for time-optimal three-axis reorientation of a rigid spacecraft;Bai X.;J. Guidance Control Dyn.,2009

2. Time-optimal three-axis reorientation of a rigid spacecraft;Bilimoria K. D.;J. Guidance Control Dyn.,1993

3. Arcminute attitude estimation for CubeSats with a novel nano star tracker;Erlank A. O.;IFAC Proc. Vol.,2014

4. Minimum-time reorientation of a rigid body;Fleming A.;J. Guidance Control Dyn.,2010

Cited by 1 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. Increasing agility in orthogonal reaction wheel attitude control systems;Acta Astronautica;2020-12