Adaptive spacecraft formation flying with actuator saturation

2010 ◽  
Vol 224 (4) ◽  
pp. 373-385 ◽  
Author(s):  
A de Ruiter
Keyword(s):  
Formation Flying ◽  
Actuator Saturation ◽  
Spacecraft Formation ◽  
Spacecraft Formation Flying

Finite-Time Coordinated Attitude Control for Spacecraft Formation Flying Under Input Saturation

2015 ◽  
Vol 137 (6) ◽  
Author(s):  
Qinglei Hu ◽  
Jian Zhang ◽  
Michael I. Friswell
Keyword(s):  
Angular Velocity ◽  
Finite Time ◽  
Attitude Control ◽  
Formation Flying ◽  
Actuator Saturation ◽  
Input Saturation ◽  
Homogeneous System ◽  
State Feedback Control ◽  
Spacecraft Formation ◽  
Spacecraft Formation Flying

In this paper, finite-time attitude coordinated control for spacecraft formation flying (SFF) subjected to input saturation is investigated. More specifically, a bounded finite-time state feedback control law is first developed with the assumption that both attitude and angular velocity signals can be measured and transmitted between formation members. Then, a bounded finite-time output feedback controller is designed with the addition of a filter, which removes the requirement of the angular velocity measurements. In both cases, actuator saturation is explicitly taken into account, and the homogeneous system method is employed to demonstrate the finite-time stability of the closed-loop system. Numerical simulation results are presented to illustrate the efficiency of the proposed control schemes.

scholarly journals Distributed Attitude Synchronization for Spacecraft Formation Flying via Event-Triggered Control

2021 ◽  
Vol 11 (14) ◽  
pp. 6299
Author(s):  
Xiong Xie ◽  
Tao Sheng ◽  
Liang He
Keyword(s):  
Control System ◽  
Formation Flying ◽  
Spacecraft Formation ◽  
Spacecraft Formation Flying ◽  
Control Scheme ◽  
Event Triggering ◽  
Computational Resources ◽  
Update Frequency ◽  
Attitude Synchronization ◽  
Event Triggered

The distributed attitude synchronization control problem for spacecraft formation flying subject to limited energy and computational resources is addressed based on event-triggered mechanism. Firstly, a distributed event-driven controller is designed to achieve attitude coordination with the limitation of energy and computing resources. Under the proposed control strategy, the controller is only updated at the event triggering instants, which effectively reduces the update frequency. Subsequently, an event-triggered strategy is developed to further decrease energy consumption and the amount of computation. The proposed event-triggered function only requires the latest state information about its neighbors, implying that the trigger threshold does not need to be calculated continuously. It is shown that the triggering interval between two successive events is strictly positive, showing that the control system has no Zeno phenomenon. Moreover, the update frequency of the proposed controller can be reduced by more than 90% compared to the update frequency of the corresponding time-driven controller with an update frequency of 10 Hz by choosing appropriate control parameters and the control system can still achieve high-precision convergence. Finally, the effectiveness of the constructed control scheme is verified by numerical simulations.

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