CN107561559A - Spinning satellite ground test program control device - Google Patents
Spinning satellite ground test program control device Download PDFInfo
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- CN107561559A CN107561559A CN201710558256.8A CN201710558256A CN107561559A CN 107561559 A CN107561559 A CN 107561559A CN 201710558256 A CN201710558256 A CN 201710558256A CN 107561559 A CN107561559 A CN 107561559A
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Abstract
The invention provides a kind of spinning satellite ground test program control device, it includes Central Processing Board and front panel, the Central Processing Board is connected with satellite, the nine class index signals that the eight class status signals for sending ten class control signals to satellite and being sent to satellite are sampled and sent to satellite measure, the front panel is connected with Central Processing Board, for receiving Central Processing Board to the sampled result of eight class status signals and lighting corresponding indicator lamp, Central Processing Board is also connected with terminal computer, for terminal computer will to be sent to the measurement result of nine class index signals, and measurement result is shown on terminal computer.The present invention possesses the test function that control signal produces, status signal sampling measures with display, index signal, check that satellite functional response and performance indications, the correctness of verifying satellites work.
Description
Technical field
The present invention relates to a kind of satellite test device, in particular it relates to a kind of spinning satellite ground test program control device.
Background technology
Spinning satellite is mainly connected during ground test by pull-off plug with ground, receives ground control signal
Control；Ground is sampled and shown in face of the status signal that satellite is sent, and index signal on star is measured, so as to examine
Satellite functional response and performance indications are looked into, obtain satellite test data, the correctness of verifying satellites work.
At present, domestic existing numerous satellite test device, a variety of test functions, but spinning satellite operation posture can be achieved
It is special, signal kinds are more, sequential relationship is complicated, there has been no a kind of satellite test device can possess control signal produce, state
The test function that signal sampling measures with display, index signal.
The present invention is exactly for a kind of satellite test device to solve the above problems.It is similar to the present invention currently without finding
The explanation or report of technology, also not yet it is collected into data similar both at home and abroad.
The content of the invention
For in the prior art the defects of, it is an object of the invention to provide a kind of spinning satellite ground test program control device,
It possesses the test function that control signal produces, status signal sampling measures with display, index signal, adapts to spinning satellite operation
The technical characterstic that posture is special, signal kinds are more, sequential relationship is complicated, can enter in satellite ground test process to satellite
Row has line traffic control, detection and status display, so as to check satellite functional response and performance indications, obtains satellite test data, tests
The correctness of satellite operation is demonstrate,proved, possesses control signal generation, the test work(of status signal sampling and display, index signal measurement
Can, it check that satellite functional response and performance indications, the correctness of verifying satellites work.
According to an aspect of the present invention, there is provided a kind of spinning satellite ground test program control device, it is characterised in that it is wrapped
Include Central Processing Board and front panel；The Central Processing Board is connected with satellite, for sending ten class control signals and right to satellite
The nine class index signals that the eight class status signals that satellite is sent are sampled and sent to satellite measure.
Preferably, the front panel is connected with Central Processing Board, for receiving Central Processing Board to eight class status signals
Sampled result simultaneously lights corresponding indicator lamp.
Preferably, the Central Processing Board is also connected with terminal computer, for by the measurement knot of nine class index signals
Fruit is sent to terminal computer, and measurement result is shown on terminal computer.
Preferably, the ten classes control signal includes the control of satellite battery break-make, the control that pull-off plug electricity takes off, protected
The logical control of shield relay, the control of scanning radiometer locking mechanism locking, apogee engine safe ignition device, safe and arm device are pulled pin
Control that control, the control of apogee engine safe ignition device, safe and arm device unblock, control system valve A2B2 are opened, the wired control of remote control
System, the control of remote-control radio, the control of satellite separation signal break-make.
Preferably, the eight classes status signal includes the logical state of the state of satellite battery break-make, pull-off plug, scanning
The state of mechanism locking, the state of release mechanism unblock, the state of release mechanism insurance, state, the priming system solution for throwing cover unblock
The state of lock, the state of remote-control radio.
Preferably, the nine class index signals sent to satellite measure the voltage, far including measuring booster
The point voltage of engine health firing device, the electric current of apogee engine safe ignition device, safe and arm device, resistance, the release mechanism of satellite
Resistance, the resistance of release mechanism unblock, resistance, control system valve A2B2 resistance, the diameter of axle of release mechanism insurance pulled pin
The resistance of tangent line bag.
Compared with prior art, the present invention has following beneficial effect：The present invention possesses control signal generation, state letter
Number sampling with display, index signal measurement test function, adapt to spinning satellite operation posture it is special, signal kinds are more, sequential
The complicated technical characterstic of relation, can have been carried out line traffic control, detection and state to satellite and shown in satellite ground test process
Show, so as to check satellite functional response and performance indications, obtain satellite test data, the correctness of verifying satellites work can
Check satellite functional response and performance indications, the correctness of verifying satellites work.
Brief description of the drawings
The detailed description made by reading with reference to the following drawings to non-limiting example, further feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is the structural representation of the present invention.
Embodiment
With reference to specific embodiment, the present invention is described in detail.Following examples will be helpful to the technology of this area
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill to this area
For personnel, without departing from the inventive concept of the premise, various modifications and improvements can be made.These belong to the present invention
Protection domain.
As shown in figure 1, spinning satellite ground test program control device of the present invention includes Central Processing Board 1 and front panel 2.
The Central Processing Board 1 is connected with satellite 3, for sending ten class control signals and to the transmission of satellite 3 to satellite 3
The nine class index signals that eight class status signals are sampled and sent to satellite 3 measure.
The front panel 2 is connected with Central Processing Board 1, for receiving sampling of the Central Processing Board 1 to eight class status signals
As a result and corresponding indicator lamp is lighted.
The Central Processing Board 1 is also connected with terminal computer 4, for will be sent to the measurement result of nine class index signals
To terminal computer 4, and measurement result is shown on terminal computer 4.
The ten classes control signal includes the control of satellite battery break-make, the control that pull-off plug electricity takes off, protection relay
What the logical control of device, the control of scanning radiometer locking mechanism locking, apogee engine safe ignition device, safe and arm device were pulled pin controls, far
The wired control of control that the control of place engine health firing device unblock, control system valve A2B2 are opened, remote control, remote control
Wireless control, the control of satellite separation signal break-make.
The eight classes status signal includes the logical state of the state of satellite battery break-make, pull-off plug, sweep mechanism lock
Fixed state, the state of release mechanism unblock, the state of release mechanism insurance, the state for throwing cover unblock, the shape of priming system unblock
State, the state of remote-control radio.
The nine class index signals sent to satellite measure voltage, apogee engine including measuring booster
The electricity that the voltage of safe ignition device, safe and arm device, the electric current of apogee engine safe ignition device, safe and arm device, resistance, the release mechanism of satellite are pulled pin
Resistance, the resistance of release mechanism unblock, the resistance of release mechanism insurance, control system valve A2B2 resistance, diameter of axle tangent line bag
Resistance.
In summary, the present invention possesses control signal generation, status signal sampling and display, the test of index signal measurement
Function, the technical characterstic that spinning satellite operation posture is special, signal kinds are more, sequential relationship is complicated is adapted to, can in satellite
In the test process of face, line traffic control, detection and status display are carried out to satellite, so as to check that satellite functional response and performance refer to
Mark, satellite test data is obtained, the correctness of verifying satellites work, satellite functional response and performance indications is check that, verifies
The correctness of satellite operation.
The specific embodiment of the present invention is described above.It is to be appreciated that the invention is not limited in above-mentioned
Particular implementation, those skilled in the art can make various deformations or amendments within the scope of the claims, this not shadow
Ring the substantive content of the present invention.
Claims (6)
1. a kind of spinning satellite ground test program control device, it is characterised in that it includes Central Processing Board and front panel；In described
Centre process plate is connected with satellite, and the eight class status signals for sending ten class control signals to satellite and being sent to satellite are adopted
Sample and the nine class index signals sent to satellite measure.
2. spinning satellite ground test program control device according to claim 1, it is characterised in that the front panel and center
Process plate is connected, for receiving Central Processing Board to the sampled result of eight class status signals and lighting corresponding indicator lamp.
3. spinning satellite ground test program control device according to claim 1, it is characterised in that the Central Processing Board is also
It is connected with terminal computer, is calculated for terminal computer will to be sent to the measurement result of nine class index signals, and in terminal
Measurement result is shown on machine.
4. spinning satellite ground test program control device according to claim 1, it is characterised in that the ten classes control signal
The logical control of the de- control of control including satellite battery break-make, pull-off plug electricity, protective relay, scanning radiometer locking
Mechanism locking control, apogee engine safe ignition device, safe and arm device pull pin control, apogee engine safe ignition device, safe and arm device solution
The wired control of control that the control of lock, control system valve A2B2 are opened, remote control, the control of remote-control radio, satellite separation signal
The control of break-make.
5. spinning satellite ground test program control device according to claim 1, it is characterised in that the eight classes status signal
The logical state of state, pull-off plug including satellite battery break-make, the state of sweep mechanism locking, the shape of release mechanism unblock
State, the state of release mechanism insurance, the state for throwing cover unblock, state, the state of remote-control radio of priming system unblock.
6. spinning satellite ground test program control device according to claim 1, it is characterised in that it is described to satellite send
Nine class index signals are measured including measuring the voltage of booster, the voltage of apogee engine safe ignition device, safe and arm device, far
Resistance that the point electric current of engine health firing device, the resistance of satellite, release mechanism are pulled pin, the resistance of release mechanism unblock,
Resistance, control system valve A2B2 resistance, the resistance of diameter of axle tangent line bag of release mechanism insurance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710558256.8A CN107561559A (en) | 2017-07-10 | 2017-07-10 | Spinning satellite ground test program control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710558256.8A CN107561559A (en) | 2017-07-10 | 2017-07-10 | Spinning satellite ground test program control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107561559A true CN107561559A (en) | 2018-01-09 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710558256.8A Pending CN107561559A (en) | 2017-07-10 | 2017-07-10 | Spinning satellite ground test program control device |
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| Country | Link |
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| CN (1) | CN107561559A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110175051A (en) * | 2019-04-11 | 2019-08-27 | 上海卫星工程研究所 | The integrated telemetering configuring management method in star ground |
| CN116395148A (en) * | 2023-03-20 | 2023-07-07 | 银河航天(北京)网络技术有限公司 | Satellite and rocket separation control system and control method |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201110880Y (en) * | 2007-10-30 | 2008-09-03 | 航天东方红卫星有限公司 | A satellite ground power supply and distribution test system |
| US20090222153A1 (en) * | 2006-06-20 | 2009-09-03 | Kara Whitney Johnson | Method of determining and controlling the inertial attitude of a spinning, artificial satellite and systems therefor |
| CN106342067B (en) * | 2006-06-13 | 2011-04-27 | 上海卫星工程研究所 | Satellite test control device |
| CN102809423A (en) * | 2012-08-10 | 2012-12-05 | 上海卫星工程研究所 | On-orbit satellite micro-vibration measurement system |
| CN105676836A (en) * | 2016-01-12 | 2016-06-15 | 上海卫星工程研究所 | Spin-up stage satellite simulation device of spin satellite |
-
2017
- 2017-07-10 CN CN201710558256.8A patent/CN107561559A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106342067B (en) * | 2006-06-13 | 2011-04-27 | 上海卫星工程研究所 | Satellite test control device |
| US20090222153A1 (en) * | 2006-06-20 | 2009-09-03 | Kara Whitney Johnson | Method of determining and controlling the inertial attitude of a spinning, artificial satellite and systems therefor |
| CN201110880Y (en) * | 2007-10-30 | 2008-09-03 | 航天东方红卫星有限公司 | A satellite ground power supply and distribution test system |
| CN102809423A (en) * | 2012-08-10 | 2012-12-05 | 上海卫星工程研究所 | On-orbit satellite micro-vibration measurement system |
| CN105676836A (en) * | 2016-01-12 | 2016-06-15 | 上海卫星工程研究所 | Spin-up stage satellite simulation device of spin satellite |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110175051A (en) * | 2019-04-11 | 2019-08-27 | 上海卫星工程研究所 | The integrated telemetering configuring management method in star ground |
| CN110175051B (en) * | 2019-04-11 | 2022-03-29 | 上海卫星工程研究所 | Satellite-ground integrated remote measurement configuration management method |
| CN116395148A (en) * | 2023-03-20 | 2023-07-07 | 银河航天(北京)网络技术有限公司 | Satellite and rocket separation control system and control method |
| CN116395148B (en) * | 2023-03-20 | 2023-09-15 | 银河航天(北京)网络技术有限公司 | Satellite and rocket separation control system and control method |
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Application publication date: 20180109 |