Real time prediction and correction of ADCS problems in LEO satellites using fuzzy logic
This approach is concerned with adapting the operations of attitude determination and control subsystem (ADCS) of low earth orbit LEO satellites through analyzing the telemetry readings received by mission control center, and then responding to ADCS off-nominal situations. This can be achieved by se...
Main Authors: | Yassin Mounir Yassin, Ahmed El Mahallawy, Abdelfattah El-Sharkawi |
---|---|
Format: | Article |
Language: | English |
Published: |
Elsevier
2017-06-01
|
Series: | Egyptian Journal of Remote Sensing and Space Sciences |
Subjects: | |
Online Access: | http://www.sciencedirect.com/science/article/pii/S1110982316300023 |
Similar Items
-
ADCS development for student CubeSat satellites – TalTech case study
by: Rauno Gordon, et al.
Published: (2021-08-01) -
Permanent Magnet Motor Design for Satellite Attitude Control With High Torque Density and Low Torque Ripple
by: Po-Huan Chou, et al.
Published: (2020-01-01) -
Passive Positioning of Flying Object With Microwave Signals From LEO Satellites: Concept and Preliminary Simulation Results
by: Defeng David Huang
Published: (2021-01-01) -
ATTITUDE GUIDANCE AND CONTROL, SIMULATION AND ANIMATION OF A LAND-SURVEY MINI-SATELLITE MOTION
by: Tatyana Somova
Published: (2016-07-01) -
LEO Precise Orbit Determination with Inter-satellite Links
by: Xingxing Li, et al.
Published: (2019-09-01)