Attitude and Orbit Control System
The cornerstone of Tensor Tech's AOCS solution is its AOCS computer, which follows industry standards to sustain space harsh environment.
The control firmware and driver can be customized especially for 3rd-party sensors and actuators that are chosen according to the mission's need.
For Positioning Devices
For Sensors
- GNSS Receiver and Antenna
- Coarse / Fine Sun Sensor
- Earth Sensor
- Star Tracker
- Magnetometer
- Inertial Measurement Unit
For Actuators
- Reaction Wheel
- Control Moment Gyroscope
- Magnetorquer
- Propulsion System
The software in AOCS computer is tailor-made and delivered according to the user's flight operation scenerios. This saves the users' time from developing and validating thier own AOCS control and estimation algorithms.
SPECIFICATIONS
- Dimensions
100 x 100 x 20 mm3
- Processor
Cortex - M7 + FPGA
- Power Consumption
Computer Core < 0.5 A @ 5 V
- Memory
1 MB Flash with ECC
2 MB MRAM
4 GB microSD - Interfaces
RS-422, RS-485, UART, I2C, SPI, CAN-FD, Ethernet, SpaceWire, and MIL-STD-1553
MAIN CONTROL BOARD
。Embedded with attitude and/or orbit control and constellation management algorithms
。Real-time sensors/actuators management
。Compatible with 3rd - party components
。> 24 krad(Si) radiation tolerance on electronics
PRODUCTS
CMG-10m-N
TensorCMG-10m-N: Integrated Version - All-in-one package seamlessly combining all essential components into a compact, unified unit.
