Visual Overview
Technical Details
Comprehensive specifications and technical information
Quick Overview
A series of highly integrated and miniaturized electronic system chips have been developed for micro- and nanosatellite control applications. These include the SoC2008 32-bit onboard application system chip, which has already been widely adopted in satellite electronic systems, and the SoC2012 32-bit onboard application system chip, designed for general onboard computing and attitude control with radiation tolerance up to 300 krad and a processing performance of 300 MIPS @ 100 MHz. The series also includes SoC2016 (LEON4 + DSP), SiP2113 general-purpose onboard computer module, and SiP2214 general-purpose onboard computing module with integrated data management functions. The SiP2115 general-purpose onboard computing module incorporates the A1013Q chip and serves as a typical onboard computer module for micro- and nanosatellites.
Key Specifications
| Parameter | Value |
|---|---|
| Specification | Details |
| --- | --- |
| Status | Space-qualified |
Key Features
- Low-cost design for high reliability
- Optoelectronic integrated architecture with high integration density
- Compact structure with low power consumption
- Strong adaptability to space environments
Applications
- Satellite systems
Documentation & Resources
Frequently Asked Questions
Common questions about The Core Components of the Micro-Satellite Controller
Which chips are included in the micro-satellite controller component series?
The series includes the SoC2008 32-bit onboard application chip, the SoC2012 32-bit chip, and the SoC2016 chip based on a LEON4 core with a DSP, complemented by SiP onboard computer modules.
What performance does the SoC2012 chip provide?
The SoC2012 32-bit onboard application chip is designed for general onboard computing and attitude control, with radiation tolerance up to 300 krad and processing performance of 300 MIPS at 100 MHz.
Which onboard computer modules are part of the series?
The series includes the SiP2113 general-purpose onboard computer module, the SiP2214 module with integrated data management, and the SiP2115 module, which incorporates the A1013Q chip.
What design characteristics define these core components?
They feature a low-cost, highly integrated optoelectronic architecture, a compact structure with low power consumption, and strong adaptability to space environments.
