Dual-Quaternion-Based Translation-Rotation-Vibration Integrated Dynamics Modeling for Flexible Spacecraft-Reference-Cited by-同舟云学术

Dual-Quaternion-Based Translation-Rotation-Vibration Integrated Dynamics Modeling for Flexible Spacecraft

Published:2019-01 Issue:1 Volume:32 Page:04018135
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sun Jun¹,Zhang Xianliang²,Wu Xiande³,Song Ting²

Affiliation:

1. Professor, Shanghai Aerospace Control Technology Institute, Shanghai Key Laboratory of Space Intelligent Control Technology, No. 1555 Zhongchun St., Shanghai 201100, P.R. China.

2. Engineer, Shanghai Aerospace Control Technology Institute, Shanghai Key Laboratory of Space Intelligent Control Technology, No. 1555 Zhongchun St., Shanghai 201100, P.R. China.

3. Associate Professor, College of Aerospace and Civil Engineering, Harbin Engineering Univ., Harbin 150001, P.R. China (corresponding author).

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.1943-5525.0000969

Reference24 articles.

1. Dual numbers representation of rigid body dynamics

2. Leader–Following Attitude Consensus for Spacecraft Formation with Rigid and Flexible Spacecraft

3. Influence of flexible appendages on dual-spin spacecraft dynamics and control

4. Vibration suppression of flexible spacecraft during attitude maneuver using CMGs

5. Dual-quaternion based distributed coordination control of six-DOF spacecraft formation with collision avoidance

Cited by 10 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. Mechanism and Application of Attitude and Orbit Coupling Dynamics for Spacecraft Proximity Relative Motion;International Journal of Aerospace Engineering;2024-05-06

2. Integrated Dynamics of Space Rigid-Flex Combination System with Time-Varying Configuration;International Journal of Aerospace Engineering;2023-09-13

3. Rigid–Flexible Coupled System Attitude–Orbit Integration Fixed-Time Control;Electronics;2023-08-03

4. A Novel Brain-inspired Architecture and Flight Experiments for Autonomous Maneuvering Flight of Unmanned Aerial Vehicles;Journal of Intelligent & Robotic Systems;2023-07-31

5. Dual-Quaternion-Based Dynamics Modeling for a Rigid–Flexible Coupling Satellite;Journal of Guidance, Control, and Dynamics;2023-07