Name | InnoSAT |
---|---|
Type | CubeSat |
Units or mass | 3U |
Status | cancelled |
Organisation | Astronautic Technology (M) Sdn. Bhd. |
Institution | Company |
Entity | Commercial |
Nation | Malaysia |
Oneliner |
Demonstrate various attitude control algorithms. |
Description |
To develop Satellite Attitude Control Systems Algorithms: Adaptive Fuzzy Logic Controller and Adaptive Parametric Black Box. Space Experimental Attitude Determination Sensors and solar Panel Sun Sensor (SEADS & SPSS). Pyramid sun sensor, magnometer, and solar panel sensory system to detect and compute body rate and attitude of Satellite. Wireless Sensor Network Payload for InnoSAT Satellite. To develop a Wireless Sensor Network that is operated from a remote location whose data is accessed via InnoSAT and transferred to the main station. Spaceborne Global Positioning System (GPS) Receiver for Autonomous Precise Timing, Positioning, and Navigation. To develop a satellite navigation and positioning system based on GPS. |
Sources | [1] [2] |
Photo Sources | [1] |
Last modified: 2022-12-29
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