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Flexible spacecraft ground control test platform and test method

A flexible spacecraft and ground control technology, applied in the aerospace field, can solve problems such as difficult ground control systems and simulation tests, and achieve good scalability

Inactive Publication Date: 2010-09-29
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to solve the problem that the existing flexible spacecraft ground control test platform is difficult to carry out realistic simulation tests on the ground control system, the invention provides a flexible spacecraft ground control test platform and test method

Method used

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  • Flexible spacecraft ground control test platform and test method
  • Flexible spacecraft ground control test platform and test method
  • Flexible spacecraft ground control test platform and test method

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Experimental program
Comparison scheme
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specific Embodiment approach 1

[0019] Specific implementation mode one: According to the instructions attached figure 1 , 2 and Figure 4 To describe this embodiment in detail,

[0020] A flexible spacecraft ground control test platform described in this embodiment includes an air-floating turntable 1, a rigid body 2, a flexible accessory 3, on-stage equipment 4, off-stage equipment 5, and a set of wireless communication devices. The lower equipment 5 includes a ground control host 5-1, a ground database 5-2 and a turntable motion measuring device 5-3, and the above-mentioned equipment 4 includes a sensor 4-1, an actuator 4-2 and an xPC master controller 4-3,

[0021] The rigid main body 2 is installed on the air bearing of the air bearing turntable 1, and the flexible accessories 3, the sensor 4-1, the actuator 4-2 and the xPC main controller 4-3 are all fixed on the rigid main body 2, and the The first communication terminal of the xPC master controller 4-3 is connected to the communication terminal o...

specific Embodiment approach 2

[0028] Specific embodiment two: this embodiment is a further description of specific embodiment one, the xPC main controller 4-3 described in the specific embodiment one includes an xPC control board 4-31, an RS232 serial port board 4-32 and A dual-port CAN board 4-33, the communication end of the xPC control board 4-31 is connected with the communication end of the RS232 serial port board 4-32 and the communication end of the dual-port CAN board 4-33 through the PC104 bus,

[0029] The xPC control board 4-31 is used to run the simulation control program, and accept the control, monitoring and online adjustment of simulation parameters of the ground control host 5-1, and return the execution result of the corresponding command, and output the sensor acquisition command through the PC104 bus at the same time and the actuator control command to the dual-port CAN board 4-33, and obtain the experimental data, and simultaneously output the experimental data to the RS232 serial port ...

specific Embodiment approach 3

[0032] Embodiment 3: The difference between this embodiment and Embodiment 1 or 2 is that Embodiment 1 or 2 also includes a lithium battery power supply, the lithium battery power supply is fixed on the rigid body 2, and the lithium battery The power signal output end of the power supply is connected to the power input end of each device in the test platform.

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Abstract

The invention relates to a flexible spacecraft ground control test platform and a test method, which relate to the field of aerospace, and solve the problem that a realistic simulated test can be performed on a ground control system difficultly by the existing flexible spacecraft ground control test platform. The test platform comprises an air flotation rotary table, a rigid main body, a flexible accessory, equipment above the rotary table and equipment under the rotary table, wherein the equipment under the rotary table comprises a ground control host, a ground database, a rotary table motion measuring device and a set of wireless communication devices; and the equipment above the rotary table comprises a sensor and an xPC main controller. The test method is implemented on the basis of the test platform. The flexible spacecraft ground control test platform and the test method lay a foundation for developing the ground control system of a flexible spacecraft.

Description

technical field [0001] The invention relates to the field of aerospace, in particular to a flexible spacecraft ground control test platform and a test method. Background technique [0002] With the development of aerospace technology, modern spacecraft often have large flexible accessories such as solar panels and antennas. There is a strong rigid-flexible coupling between the central rigid body and flexible appendages of this type of flexible spacecraft, which is difficult to describe mathematically accurately. For this type of complex spacecraft with flexible accessories, due to the particularity of its operating environment, high risk, high cost, and high precision and high complexity of the control system, it is not enough for the control system scheme to be simulated only through numerical simulation. A full semi-physical simulation test of the satellite control system must be done before going to the sky to verify the stability of the system design, modify the system ...

Claims

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Application Information

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IPC IPC(8): G05B23/02
Inventor 孔宪仁杨正贤张锦绣董晓光叶东陈雪琴廖俊徐大富许海玉
Owner HARBIN INST OF TECH
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