CN108803306A - Mars probes day insults overall process and manages independently method - Google Patents
Mars probes day insults overall process and manages independently method Download PDFInfo
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- CN108803306A CN108803306A CN201810683930.XA CN201810683930A CN108803306A CN 108803306 A CN108803306 A CN 108803306A CN 201810683930 A CN201810683930 A CN 201810683930A CN 108803306 A CN108803306 A CN 108803306A
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D3/00—Control of position or direction
- G05D3/12—Control of position or direction using feedback
Abstract
The present invention provides insulting overall process a kind of Mars probes day to manage independently method, include the following steps：Step 1：Comprehensive electricity subsystem receives parameter and confirms after instruction the time on detector, if the value of continuous three beats is all higher than targeting criteria, then it is assumed that have been enter into and day insult the stage；Step 2：It is often to close that comprehensive electricity subsystem, which sends instruction all load are arranged,；Step 3：Tracking-telemetry and command subsystem switches to the remote control of uplink low-gain antenna, downlink low-gain antenna telemetering；Step 4：It is controlled using wheel and carries out attitude maneuver, gone to and day is slightly oriented.The present invention is not necessarily to earth station's wireless remotecontrol before and after insulting event day and occurring; Mars independently carries out pattern switching around device; ensure that Mars smoothly switches Summer Solstice or the Winter Solstice icepro operating mode around device when day icepro occurs; the safe operation during day insults; science can be smoothly switched to after insulting day around section normal mode of operation, it is ensured that Mars probes safe and stable operation in meeting with day icepro event procedure.
Description
Technical field
The present invention relates to a kind of autonomous management methods, and in particular, to insults a kind of Mars probes day overall process from being responsible for
Reason method.
Background technology
When Mars runs on the position of approximate same straight line around device, the sun, earth ground stations, the powerful electricity of the sun
For magnetic radiation to causing to interfere strongly around the signal of communication of device, the phenomenon on this communications field is known as day icepro.During day insults,
The nonuniform broad-band noise that the sun generates to device can generate interference by communication path, cause the earth and Mars logical between device
It is unreliable to believe.For the Mars probes around mars, it is that Mars probes can not during in orbit to insult day
The special event avoided.Operating mode is insulted in order to ensure detector can smoothly enter into day, the safe operation in day insulting overall process, day
Normal mode of operation can be smoothly switched to after icepro, need targetedly to formulate a suitable mars exploration day icepro overall process
Autonomous management method.Currently, deep space probe mainly uses earth station to carry out operational management by means such as wireless remotecontrols.
During day insults, the powerful electromagnetic radiation of the sun can generate strong interference to Mars around the radio signal of device.Therefore, in day
During icepro, traditional earth station's remote control means will be unable to implement effectively remote control around device to Mars, will face risk out of control.
Invention content
For the defects in the prior art, the object of the present invention is to provide insult overall process a kind of Mars probes day from supervisor
Reason method is not necessarily to earth station's wireless remotecontrol before and after insulting event day and occurring, and Mars independently carries out pattern switching around device, really
It protects Mars and smoothly switches Summer Solstice or the Winter Solstice icepro operating mode, the safe operation during day insults, after day insults when day icepro occurs around device
Science can smoothly be switched to around section normal mode of operation, it is ensured that Mars probes are safe, steady in meeting with day icepro event procedure
Fixed operation.
According to an aspect of the present invention, a kind of Mars probes day icepro overall process autonomous management method, feature are provided
It is, includes the following steps：
Step 1：Comprehensive electricity subsystem receives parameter and confirms after instruction the time on detector, if the value of continuous three beats
It is all higher than targeting criteria, then it is assumed that have been enter into and day insult the stage；
Step 2：It is often to close that comprehensive electricity subsystem, which sends instruction all load are arranged,；
Step 3：Tracking-telemetry and command subsystem switches to the remote control of uplink low-gain antenna, downlink low-gain antenna telemetering；
Step 4：It is controlled using wheel and carries out attitude maneuver, gone to and day is slightly oriented；
Step 5：After the completion of attitude maneuver, solar wing goes to day and keeps；
Step 6：It is comprehensive electricity subsystem retransmit instruction switching thermal control, propulsion, directional aerial, power subsystem Working mould
The formula Summer Solstice or the Winter Solstice insults pattern；
Step 7：During day insults, detector is remained to day pattern, and independently carries out jet flywheel unloading；The sun
Wing driving was kept to day, and high-gain aerial driving is kept over the ground；Earth station continues empty to being sent around device uplink in visible segmental arc
Telecommand is operated, the time around the received non-operation instruction of device record and serial number；Meanwhile around device continue under pass it is distant
It surveys；
Step 8：After reaching out icepro moment day, earth station counts communication among unit success rate, if more than targeting criteria, then
Earth station's uplink, which is sent out, insults pattern switching instruction day；
Step 9：After comprehensive electricity subsystem receives instruction, posture, which is adopted, switches to accurate Direct to the sun pattern；
Step 10：Tracking-telemetry and command subsystem switches to high-gain aerial operating mode；
Step 11：Earth station completes after measuring rail, upper note orbit parameter；
Step 12：Mars probes integrated electronics send instruction switching thermal control, propulsion, directional aerial, power subsystem
Operating mode to normal mode of operation.
Preferably, the step 1 is introduced into high-gain TT & C before entering icepro stage day.
Compared with prior art, the present invention has following advantageous effect：The present invention is not necessarily to before and after insulting event day and occurring
Earth station's wireless remotecontrol, Mars independently carry out pattern switching around device, it is ensured that Mars is smoothly cut around device when day icepro occurs
It shifts to and day insults operating mode, the safe operation during day insults can smoothly switch to science after insulting day and be worked normally around section
Pattern, it is ensured that Mars probes safe and stable operation in meeting with day icepro event procedure.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is the schematic diagram for Mars probes day of the present invention insulting that overall process manages independently method.
Specific implementation mode
With reference to specific embodiment, the present invention is described in detail.Following embodiment will be helpful to the technology of this field
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill of this field
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.
Include the following steps as shown in Figure 1, insulting overall process autonomous management method Mars probes day of the present invention：
Step 1：Comprehensive electricity subsystem receives parameter and confirms after instruction the time on detector, if the value of continuous three beats
It is all higher than targeting criteria (TJRL), then it is assumed that have been enter into and day insult the stage；
Step 2：It is often to close that comprehensive electricity subsystem, which sends instruction all load are arranged,；
Step 3：Tracking-telemetry and command subsystem switches to the remote control of uplink low-gain antenna, downlink low-gain antenna telemetering；
Step 4：It is controlled using wheel and carries out attitude maneuver, gone to and day is slightly oriented；
Step 5：After the completion of attitude maneuver, solar wing goes to day and keeps；
Step 6：Comprehensive electricity subsystem retransmits the work of the subsystems such as instruction switching thermal control, propulsion, directional aerial, power supply
The pattern Summer Solstice or the Winter Solstice insults pattern；
Step 7：During day insults, detector is remained to day pattern, and independently carries out jet flywheel unloading；The sun
Wing driving was kept to day, and high-gain aerial driving is kept over the ground；Earth station continues empty to being sent around device uplink in visible segmental arc
Telecommand is operated, the time around the received non-operation instruction of device record and serial number；Meanwhile around device continue under pass it is distant
It surveys；
Step 8：After reaching out icepro moment day, earth station counts communication among unit success rate, if more than targeting criteria, then
Earth station's uplink, which is sent out, insults pattern switching instruction day；
Step 9：After comprehensive electricity subsystem receives instruction, posture, which is adopted, switches to accurate Direct to the sun pattern；
Step 10：Tracking-telemetry and command subsystem switches to high-gain aerial operating mode；
Step 11：Earth station completes after measuring rail, upper note orbit parameter；
Step 12：Mars probes integrated electronics send instruction switching thermal control, propulsion, directional aerial, power supply etc. point
The operating mode of system is to normal mode of operation.
Step 1 is introduced into high-gain TT & C so that it is convenient to carry out observing and controlling and judgement before entering icepro stage day.
The present invention is not necessarily to earth station's wireless remotecontrol before and after insulting event day and occurring, and Mars independently carries out pattern around device and cuts
It changes, it is ensured that Mars smoothly switches Summer Solstice or the Winter Solstice icepro operating mode around device when day icepro occurs, and day is insulted knot in the safe operation during day insults
Shu Houneng smoothly switches to science around section normal mode of operation, it is ensured that Mars probes are pacified in meeting with day icepro event procedure
Entirely, stable operation.
Specific embodiments of the present invention are 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 (2)
1. a kind of Mars probes day insults overall process and manages independently method, which is characterized in that include the following steps：
Step 1：Comprehensive electricity subsystem receives parameter and confirms after instruction the time on detector, if the value of continuous three beats is big
In targeting criteria, then it is assumed that have been enter into and day insult the stage；
Step 2：It is often to close that comprehensive electricity subsystem, which sends instruction all load are arranged,；
Step 3：Tracking-telemetry and command subsystem switches to the remote control of uplink low-gain antenna, downlink low-gain antenna telemetering；
Step 4：It is controlled using wheel and carries out attitude maneuver, gone to and day is slightly oriented；
Step 5：After the completion of attitude maneuver, solar wing goes to day and keeps；
Step 6：It is comprehensive electricity subsystem retransmit instruction switching thermal control, propulsion, directional aerial, power subsystem operating mode extremely
Day insults pattern；
Step 7：During day insults, detector is remained to day pattern, and independently carries out jet flywheel unloading；Solar wing drives
Dynamic to keep to day, high-gain aerial driving is kept over the ground；Earth station continues to send do-nothing operation to around device uplink in visible segmental arc
Telecommand, the time around the received non-operation instruction of device record and serial number；Meanwhile it surrounding under device continues and passing telemetering；
Step 8：After reaching out day and insulting the moment, earth station counts communication among unit success rate, if more than targeting criteria, then ground
Uplink of standing, which is sent out, insults pattern switching instruction day；
Step 9：After comprehensive electricity subsystem receives instruction, posture, which is adopted, switches to accurate Direct to the sun pattern；
Step 10：Tracking-telemetry and command subsystem switches to high-gain aerial operating mode；
Step 11：Earth station completes after measuring rail, upper note orbit parameter；
Step 12：Mars probes integrated electronics send instruction switching thermal control, propulsion, directional aerial, power subsystem work
Operation mode is to normal mode of operation.
2. Mars probes day according to claim 1 insults overall process and manages independently method, which is characterized in that the step
One is introduced into high-gain TT & C before entering icepro stage day.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201810683930.XA CN108803306B (en) | 2018-06-28 | 2018-06-28 | Mars detector day-to-day whole-process autonomous management method |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810683930.XA CN108803306B (en) | 2018-06-28 | 2018-06-28 | Mars detector day-to-day whole-process autonomous management method |
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| CN108803306A true CN108803306A (en) | 2018-11-13 |
| CN108803306B CN108803306B (en) | 2021-05-11 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113176072A (en) * | 2021-03-30 | 2021-07-27 | 上海卫星工程研究所 | General analysis method suitable for detecting constellation sunlight interference to earth optics |
| CN113472418A (en) * | 2021-06-01 | 2021-10-01 | 航天科工空间工程发展有限公司 | Method for realizing inter-satellite link sun-slush forecasting by ground operation control system |
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| US705970A (en) * | 1901-11-14 | 1902-07-29 | Orville F Shattuck | Solar attachment for transit instruments. |
| CN1126398A (en) * | 1994-09-27 | 1996-07-10 | 现代电子产业株式会社 | Method for recovering from sun transit in communication of very small aperture terminal |
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2018
- 2018-06-28 CN CN201810683930.XA patent/CN108803306B/en active Active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US705970A (en) * | 1901-11-14 | 1902-07-29 | Orville F Shattuck | Solar attachment for transit instruments. |
| CN1126398A (en) * | 1994-09-27 | 1996-07-10 | 现代电子产业株式会社 | Method for recovering from sun transit in communication of very small aperture terminal |
Non-Patent Citations (3)
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| P. TANGA.ETAL: "The aureole of Venus: light refraction in the mesosphere", 《EPSC-DPS JOINT MEETING 2011》 * |
| 奚小瑾: "日凌对转发式卫星测定轨的影响研究", 《中国硕士学位论文全文数据库（电子期刊）》 * |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113176072A (en) * | 2021-03-30 | 2021-07-27 | 上海卫星工程研究所 | General analysis method suitable for detecting constellation sunlight interference to earth optics |
| CN113472418A (en) * | 2021-06-01 | 2021-10-01 | 航天科工空间工程发展有限公司 | Method for realizing inter-satellite link sun-slush forecasting by ground operation control system |
| CN113472418B (en) * | 2021-06-01 | 2022-04-19 | 航天科工空间工程发展有限公司 | Method for realizing inter-satellite link sun-slush forecasting by ground operation control system |
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