Satellite formation flying control design based on hybrid control system stability analysis

2000 ◽  
Author(s):  
R.K. Yedavalli ◽  
A.G. Sparks
Keyword(s):  
Control System ◽  
Stability Analysis ◽  
Formation Flying ◽  
Hybrid Control ◽  
Control Design ◽  
System Stability ◽  
Satellite Formation Flying ◽  
Satellite Formation ◽  
System Stability Analysis ◽  
Hybrid Control System

scholarly journals TRACKING CONTROL DESIGN USING SLIDING MODE TECHNIQUES FOR SATELLITE FORMATION FLYING

2003 ◽  
Vol 20 (4) ◽  
pp. 365-374 ◽  
Author(s):  
Hyung-Chul Lim ◽  
Hyo-Choong Bang ◽  
Kwan-Dong Park ◽  
Pil-Ho Park
Keyword(s):  
Tracking Control ◽  
Formation Flying ◽  
Sliding Mode ◽  
Control Design ◽  
Satellite Formation Flying ◽  
Satellite Formation

Power System Stability Analysis Using Feedback Control System Modeling Including HVDC Transmission Links

2016 ◽  
Vol 31 (1) ◽  
pp. 116-124 ◽  
Author(s):  
Ali Bidadfar ◽  
Hans-Peter Nee ◽  
Lidong Zhang ◽  
Lennart Harnefors ◽  
Sanaz Namayantavana ◽  
...  
Keyword(s):  
Control System ◽  
Stability Analysis ◽  
Feedback Control ◽  
Power System ◽  
System Modeling ◽  
Power System Stability ◽  
System Stability ◽  
Feedback Control System ◽  
Hvdc Transmission ◽  
System Stability Analysis

Satellite formation flying using an innovative autonomous control system (AutoCon) environment

1997 ◽  
Author(s):  
Frank Bauer ◽  
John Bristow ◽  
David Folta ◽  
Kathy Hartman ◽  
David Quinn ◽  
...  
Keyword(s):  
Control System ◽  
Formation Flying ◽  
Autonomous Control ◽  
Satellite Formation Flying ◽  
Satellite Formation

The Application of LabVIEW in Control System Stability Analysis

2012 ◽  
Vol 182-183 ◽  
pp. 788-792
Author(s):  
Xue Ning Xing
Keyword(s):  
Control System ◽  
Stability Analysis ◽  
User Interface ◽  
Control Theory ◽  
Time Domain ◽  
System Stability ◽  
Graphic User Interface ◽  
System Stability Analysis ◽  
The Stability ◽  
Classical Control

The stability of the system is the prior condition for whether the control system can operate normally, in the classical control theory, time domain analyze method, complex domain analyze method and frequency domain analyze method are often used to analyze the performance of the control system. Using LabVIEW to design graphic user interface, input parameters, then the curve can be drawn out immediately and calculate the interrelated parameters, which plays an important role in analyzing the stability of the system.

Fault Tolerant Guidance of Under-Actuated Satellite Formation Flying Using Inter-Vehicle Coulomb Force

2019 ◽  
Vol 2 (1) ◽  
pp. 43-52
Author(s):  
Alireza Alikhani ◽  
Safa Dehghan M ◽  
Iman Shafieenejad
Keyword(s):  
Fault Tolerance ◽  
Formation Flying ◽  
Fault Tolerant ◽  
Coulomb Force ◽  
Control Law ◽  
Triangular Form ◽  
Satellite Formation Flying ◽  
Satellite Formation ◽  
Guidance Law ◽  
Tolerance Approach

In this study, satellite formation flying guidance in the presence of under actuation using inter-vehicle Coulomb force is investigated. The Coulomb forces are used to stabilize the formation flying mission. For this purpose, the charge of satellites is determined to create appropriate attraction and repulsion and also, to maintain the distance between satellites. Static Coulomb formation of satellites equations including three satellites in triangular form was developed. Furthermore, the charge value of the Coulomb propulsion system required for such formation was obtained. Considering Under actuation of one of the formation satellites, the fault-tolerance approach is proposed for achieving mission goals. Following this approach, in the first step fault-tolerant guidance law is designed. Accordingly, the obtained results show stationary formation. In the next step, tomaintain the formation shape and dimension, a fault-tolerant control law is designed.

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