Active vibration suppression in flexible spacecraft with optical measurement
Z Wang, Y Jia, S Xu, L Tang - Aerospace Science and Technology, 2016 - Elsevier
With the development of the space station technology in China, the active vibration
suppression of the lager flexible antennas and solar panels that mounted on the space …
suppression of the lager flexible antennas and solar panels that mounted on the space …
Vibration suppression-based attitude control for flexible spacecraft
Z Wang, M Xu, Y Jia, S Xu, L Tang - Aerospace Science and Technology, 2017 - Elsevier
In this paper, a novel approach for high-accuracy attitude control in a flexible spacecraft is
developed by compensating and damping the vibration of the flexible appendage. A …
developed by compensating and damping the vibration of the flexible appendage. A …
Active vibration suppression of flexible spacecraft during attitude maneuver with actuator dynamics
S Xu, N Cui, Y Fan, Y Guan - IEEE Access, 2018 - ieeexplore.ieee.org
A novel active vibration suppression approach based on a flywheel actuator for flexible
spacecraft during attitude maneuvering is proposed in this paper. The flywheel is regarded …
spacecraft during attitude maneuvering is proposed in this paper. The flywheel is regarded …
Fuzzy attitude control of solar sail via linear matrix inequalities
J Baculi, MA Ayoubi - Acta Astronautica, 2017 - Elsevier
This study presents a fuzzy tracking controller based on the Takagi-Sugeno (TS) fuzzy
model of the solar sail. First, the TS fuzzy model is constructed by linearizing the existing …
model of the solar sail. First, the TS fuzzy model is constructed by linearizing the existing …
Attitude control of a flexible spacecraft via fuzzy optimal variance technique
C Sendi - Mathematics, 2022 - mdpi.com
This paper investigates the performance of a fuzzy optimal variance control technique for
attitude stability and vibration attenuation with regard to a spacecraft made of a rigid platform …
attitude stability and vibration attenuation with regard to a spacecraft made of a rigid platform …
Robust-optimal fuzzy model-based control of flexible spacecraft with actuator constraint
This paper presents a robust-optimal fuzzy controller for position and attitude stabilization
and vibration suppression of a flexible spacecraft during antenna retargeting maneuver. The …
and vibration suppression of a flexible spacecraft during antenna retargeting maneuver. The …
Aerodynamic drag analysis of 3-DOF flex-gimbal GyroWheel system in the sense of ground test
GyroWheel is an innovative device that combines the actuating capabilities of a control
moment gyro with the rate sensing capabilities of a tuned rotor gyro by using a spinning flex …
moment gyro with the rate sensing capabilities of a tuned rotor gyro by using a spinning flex …
[PDF][PDF] Fuzzy attitude control of solar sail with translating control masses via linear matrix inequalities
J Baculi, MA Ayoubi - AAS/AIAA Space Flight Mechanics Meeting, 2016 - researchgate.net
We present a fuzzy model-based attitude controller for a solar-sail. First, a Takagi-Sugeno
fuzzy model of solar-sail is derived based on the existing equations of motion. Then, by …
fuzzy model of solar-sail is derived based on the existing equations of motion. Then, by …
[HTML][HTML] 漂浮基转台线性化状态反馈指向与跟踪控制
赵国伟, 王伟民, 方艺忠, 王灏宇 - 北京航空航天大学学报, 2015 - bhxb.buaa.edu.cn
在空间漂浮平台上, 两自由度转台在跟踪指向空间目标的过程中对平台会产生姿态扰动,
使平台姿态发生变化, 从而影响转台末端的空间指向, 降低指向跟踪精度, 因此转台与平台间存在 …
使平台姿态发生变化, 从而影响转台末端的空间指向, 降低指向跟踪精度, 因此转台与平台间存在 …
[PDF][PDF] Attitude Control of a Flexible Spacecraft via Fuzzy Optimal Variance Technique. Mathematics 2022, 10, 179
C Sendi - 2022 - academia.edu
This paper investigates the performance of a fuzzy optimal variance control technique for
attitude stability and vibration attenuation with regard to a spacecraft made of a rigid platform …
attitude stability and vibration attenuation with regard to a spacecraft made of a rigid platform …