Digital satellite interface bias verification system
A technology of digital interface and verification system, which is applied in the field of verification of the input and output characteristics of satellite digital interfaces, can solve problems such as inability to adjust, cannot set multiple digital signal delay relationships, and cannot grasp the interface tolerance characteristics, etc., to achieve real-time effect of change
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2012-01-18
Smart Images
Figure 1 Figure 2 Figure 3
Abstract
Description
technical field
[0001] The invention relates to a satellite digital interface deviation verification system, which is suitable for verification of the input and output characteristics of the satellite digital interface. Background technique
[0002] At present, many digital transmission interfaces are used in domestic high-orbit communication satellite measurement and control subsystems, which are used to transmit telemetry signals and remote control commands between different stand-alone machines.
[0003] High-orbit communication satellites mainly use serial interfaces to realize digital signal transmission, and data signals are transmitted according to the specified timing and level. A more commonly used transmission form is: the telemetry acquisition terminal outputs a strobe signal and a clock signal, and the acquired terminal outputs serial telemetry data shifted according to the clock signal after the strobe signal arrives. For the telemetry acquisition end, it is ne...
Examples
Embodiment Construction
[0029] Specific embodiments of the present invention will be further described in detail below in conjunction with the accompanying drawings.
[0030] The invention provides a satellite digital interface deflection verification system, which is used for artificially deflecting signals input to satellite equipment during ground testing, so that the tolerance characteristics of the satellite interface can be tested on the ground. Such as figure 1 Shown is the composition of the system of the present invention, which mainly consists of the following modules: clock module, host computer interface module, FPGA, on-star interface module and power supply module;
[0031] In the present invention, FPGA uses 3.5 million gate chips VERTEX4 of XILINX company TM XC4VSX35, the corresponding configuration FLASH is XCF32PVO48C, the capacity is 32Mbit, and the package is VO48. The configuration mode of FPGA and Flash is the most basic main serial configuration mode, and the clock of FPGA is...