Direct Force Sliding Mode Attitude Control based on Fully Actuated System Theory-Reference-Cited by-同舟云学术

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Direct Force Sliding Mode Attitude Control based on Fully Actuated System Theory

Published:2023-07-14 Issue: Volume: Page:
ISSN:
Container-title:2023 2nd Conference on Fully Actuated System Theory and Applications (CFASTA)
language:
Short-container-title:

Author:

Huang Yixin¹,Chang Qi¹,Zhou Yiwen¹,Xia Bin¹,Jin Yihuan¹

Affiliation:

1. Shanghai Aerospace Control Technology Institute,Shanghai,China,201109

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10243163/10243123/10243319.pdf?arnumber=10243319

Reference11 articles.

1. Quantitative Analysis of Influence Factor of Guidance Accuracy for Air-Defense Missiles [J];fu;Flight Control & Detection,2020

2. Impulse Control Law of KKV Attitude Control Based on Digital Mutative Moment [J];zang;Ordnance Industry Automation,2018

3. High-order System Approaches:I. Fully-actuated Systems and Parametric Designs[J];guang-ren;ACTA Automatica Sinica,2020

4. Application Simulation of Pulse Modulation in Small Attitude Control Thruster[J];qian,2017

5. Spacecraft vibration reduction using pulse-width pulse-frequency modulated input shaper

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