| Name | InnoSAT |
|---|---|
| Spacecraft type | CubeSat |
| Units or mass | 3U |
| Status | cancelled |
| Organisation | ATSB (Astronautic Technology Sdn Bhd) |
| Institution | Company |
| Entity | Commercial |
| Headquarters | Malaysia |
| Partners | Universiti Sains Malaysia (USM), Universiti Teknologi Malaysia (UTM) and Universiti Malaysia Perlis (UniMAP). |
| 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: 2024-05-29
