A Fully-Modular Coupling Kit Enabling OSAM, Exploration and Beyond: iSSI - The intelligent Space System Interface by iBOSS

2021 ◽  
Author(s):  
Joerg Kreisel ◽  
Thomas A. Schervan ◽  
Dennis R. Wingo
Keyword(s):  
Space System ◽  
Intelligent Space

scholarly journals Sensor Systems for Vehicle Environment Perception in a Highway Intelligent Space System

Sensors ◽  
2014 ◽  
Vol 14 (5) ◽  
pp. 8513-8527 ◽  
Author(s):  
Xiaofeng Tang ◽  
Feng Gao ◽  
Guoyan Xu ◽  
Nenggen Ding ◽  
Yao Cai ◽  
...  
Keyword(s):  
Sensor Systems ◽  
Space System ◽  
Intelligent Space ◽  
Environment Perception

An Intelligent Space System and its Communication Method to Achieve the Low Energy Consumption

2016 ◽  
Vol 136 (12) ◽  
pp. 1804-1814
Author(s):  
Shoichi Okazaki ◽  
Toru Watanabe ◽  
Masahiro Higuchi ◽  
Akiko Watanabe ◽  
Tetsuo Shiozuki ◽  
...  
Keyword(s):  
Energy Consumption ◽  
Low Energy ◽  
Space System ◽  
Intelligent Space ◽  
Communication Method ◽  
Low Energy Consumption

Dynamics of a deformed space system of bodies with programmed change of the configuration

2004 ◽  
Vol 10 (1) ◽  
pp. 45-53 ◽  
Author(s):  
V.I. Dranovsky ◽  
◽  
A.E. Zakrzhevskii ◽  
V.S. Khoroshylov ◽  
◽  
...  
Keyword(s):  
Space System

The problem of ballistic design of the space system Earth remote sensing in stable near-circular sun-synchronous orbits with long-term spacecraft lifetime

2018 ◽  
pp. 3-9
Author(s):  
V. M. Artyushenko ◽  
D. Y. Vinogradov
Keyword(s):  
Remote Sensing ◽  
Target Function ◽  
Normal Operation ◽  
Space Systems ◽  
Light Conditions ◽  
Space System ◽  
Earth Remote Sensing ◽  
Synchronous Orbit ◽  
Favorable Conditions

The article deals with the issues related to the problem of ballistic design of the space system of remote sensing of the Earth on stable near-circular solar-synchronous orbits with long-term existence of spacecraft. We propose a rational method of maintaining a solar-synchronous orbit in given light conditions with prolonged active lifetime of space systems. In solving this problem, the total time of normal operation of the system for a given period of operation, during which the most favorable conditions for the use of spacecraft are provided on the main parts of orbits, is taken as a target function.

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