Stellar/inertial (EBCCD/MEMS) attitude measurement and control of small satellites

2001 ◽  
Author(s):  
Richard Phillips ◽  
William Johnson
1987 ◽  
Vol 20 (5) ◽  
pp. 89-101
Author(s):  
P. Bourg ◽  
B. Cyna ◽  
Y. Martinet ◽  
E. Brüderle ◽  
T. Bückle ◽  
...  

2012 ◽  
Vol 503 ◽  
pp. 393-396
Author(s):  
Shao Peng Liu ◽  
Zhao Ying Zhou ◽  
Xing Yang ◽  
Qiu Sheng Liu ◽  
Qiong Wang ◽  
...  

The Modular Platform System in this Paper Consists of a Series of Modularized MEMS Subsystems, Including Central Control Unit, MEMS Attitude Measurement Unit, Environment Unit, Flight Measurement and Control Unit, Time Control Unit, Impact Vibration Measurement Unit and other Auxiliary Modular Units. the Key of the System Is the MEMS Attitude Measurement Unit, which Can Resolve the Real Time Attitude Information of the Carrier. the System Platform Chooses Different Sensors and Units According to Various Circumstances and Implements Data Collection, Fusion and Solution through the Central Processing Module. by Means of Carrying Distinct Units, System Platform Can Constitute many Measurement Control Systems, such as Micro Wireless Attitude Determination System, MAV Flight Data Recorder, MAV Flight Control System and PHM (prognostic and Health Management). with Application of MEMS, the System in this Paper Is High-Efficient, Low-Weighted, Simple-Structured, High-Reliable and even Can Respond in a Short Time. in View of these Merits, the System Can Be Applied in many Kinds of Attitude Measurement and Control System.


2021 ◽  
Vol 233 ◽  
pp. 04041
Author(s):  
Chen Chao ◽  
Wang ShuYi ◽  
Liu Jie ◽  
Wu Sen Tang

With the rapid development of the national economy, the digital city and smart city have become the development trends of China’s urbanization, proposing higher and higher requirements for earth mapping. The emergence of high-resolution mapping satellites has satisfied the demand for national economic development. Since China’s first satellite measuring scale of 1:10,000 was launched in 2019, thus GF-7 satellite has realized the arc-second attitude measurement accuracy, where the degree of stability reached 10- 5°/s. Based on the author’s multi-year research on the design of high-resolution satellite control system, the key technologies and design methods for the high-precision attitude measurement and control system were expounded, the validation results were explained, and the future direction for improving the control precision of the high-resolution mapping satellite was proposed in the end.


2001 ◽  
Author(s):  
G. Mainelis ◽  
R. Gorny ◽  
K. Willeke ◽  
S. Grinshpun ◽  
T. Reponen ◽  
...  

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