.jpg "ZDPS 1A")
| Spacecraft | ZDPS 1A |
|---|---|
| Spacecraft type | Nanosatellite |
| Units or mass | 3.5 kg |
| Organisation | Zhejiang University |
| Institution | University |
| Entity | Academic / Education |
| Headquarters | China |
| Oneliner |
Demonstrate platform technologies with focus on camera, COTS components and ADCS. |
| Description |
Platform verification. The space environmental adaption and application of the various parts including the miniaturized commercial-off-the-shelf (COTS) MEMS accelerometers and gyroscopes, the in-house-developed panoramic CMOS camera and the novel tri-junction solar cells were to be experimented. Attitude determination and control experimentation. The correctness and effectiveness of the attitude determination and control scheme were to be evaluated via attitude de-tumbling and stabilizing experiments. Micro panoramic camera. Momentum wheel is employed to offer gyro stiffness stability in the pitch. |
| Sources | [1] |
| Photo sources | [1] [2] |
| Space photos | 
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Related Spacecraft
| Name | Status | Launcher | Launch date | Orbit |
|---|---|---|---|---|
| ZDPS 1A 01 (Zheda Pixing, Pixing 1) | Was operational until XXXX-XX-XX, more than 2 years? | Long March 2D | 2010-09-22 | 650 km, 98.2 deg |
| ZDPS 1A 02 (Zheda Pixing, Pixing 1) | Was operational until XXXX-XX-XX, more than 2 years? | Long March 2D | 2010-09-22 | 650 km, 98.2 deg |
Last modified: 2024-05-29
