scholarly journals “Flyable” Guidance and Control Algorithms for Orbital Rendezvous Maneuver

2018 ◽  
Vol 11 (1) ◽  
pp. 14-24 ◽  
Author(s):  
Elisa CAPELLO ◽  
Fabrizio DABBENE ◽  
Giorgio GUGLIERI ◽  
Elisabetta PUNTA
Author(s):  
Ye.I. Somov ◽  
◽  
S.A. Butyrin ◽  
S.Ye. Somov ◽  
◽  
...  

The control problems on a space robot during its approach to an information geostationary satellite are considered. The robot motion control system uses an electric propulsion system with 8 engines at the pulse-width modulation of their thrust values and a gyroscopic moment cluster based on 4 gyrodines with digital control. Numerical results are presented that demonstrate the effectiveness of the developed discrete guidance and control algorithms.


Author(s):  
Jody Davis ◽  
Alicia Dwyer Cianciolo ◽  
Richard Powell ◽  
Jeremy Shidner ◽  
Eduardo Garcia-Llama

2016 ◽  
Vol 2016 ◽  
pp. 1-14 ◽  
Author(s):  
Matteo Dentis ◽  
Elisa Capello ◽  
Giorgio Guglieri

The purpose of this paper is the design of guidance and control algorithms for orbital space maneuvers. A 6-dof orbital simulator, based on Clohessy-Wiltshire-Hill equations, is developed in C language, considering cold gas reaction thrusters and reaction wheels as actuation system. The computational limitations of on-board computers are also included. A combination of guidance and control algorithms for an orbital maneuver is proposed: (i) a suitably designed Zero-Effort-Miss/Zero-Effort-Velocity (ZEM/ZEV) algorithm is adopted for the guidance and (ii) a linear quadratic regulator (LQR) is used for the attitude control. The proposed approach is verified for different cases, including external environment disturbances and errors on the actuation system.


Author(s):  
Ye.I. Somov ◽  
◽  
S.A. Butyrin ◽  
T.Ye. Somova ◽  
◽  
...  

Methods for guidance and motion control of a space robot during a flyby of a geostationary satellite at a visual monitoring its technical state are considered. Numerical results are presented that demonstrate the effectiveness of the developed discrete guidance and control algorithms.


2021 ◽  
Vol 122 ◽  
pp. 100696
Author(s):  
Runqi Chai ◽  
Antonios Tsourdos ◽  
Al Savvaris ◽  
Senchun Chai ◽  
Yuanqing Xia ◽  
...  

Author(s):  
S.Ye. Somov ◽  
◽  
T.Ye. Somova ◽  
◽  

Methods for guidance and motion control of a space robot during a flyby of a geostationary satellite at a visual monitoring its technical state are considered. Numerical results are presented that demonstrate the effectiveness of the developed discrete guidance and control algorithms.


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