CN201040587Y - Solar energy lunar excursion vehicle - Google Patents
Solar energy lunar excursion vehicle Download PDFInfo
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- CN201040587Y CN201040587Y CNU2007200681287U CN200720068128U CN201040587Y CN 201040587 Y CN201040587 Y CN 201040587Y CN U2007200681287 U CNU2007200681287 U CN U2007200681287U CN 200720068128 U CN200720068128 U CN 200720068128U CN 201040587 Y CN201040587 Y CN 201040587Y
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Abstract
The utility model discloses a solar energy lunar landing vehicle, comprising a main control center module, a communication launcher, an energy supply module, a visual recognition module, a sampling drilling module, a sample storage chamber, and a suspension marching system. The lunar landing vehicle also has an aircraft. A detector is installed on the aircraft and the lunar landing vehicle is provided with an aircraft parking device for parking the aircraft. The solar energy lunar landing vehicle can realize the purpose of accurate measuring and analyzing the data and sample through introducing a flight detector with smaller price and lower cost under the complicated environment and unpredictable lunar detecting status, also avoid certain defects brought by participation of the astronaut.
Description
Technical field
The utility model relates to a kind of solar power lunar rover vehicle.
Background technology
The moon is as the unique natural satellite of the earth, very close with the relation of the earth, Lunar Probe Project is as the part of various countries' space program, its meaning for whole space probation is equally very great, the just said moon exploration remote control robot of the lunar rover vehicle, as travelling at moonscape and the moon being investigated and the special-use vehicle of collection analysis sample, the performance that it had also directly has influence on the result and the efficient of whole detection, the existing lunar rover vehicle is divided into the unmanned lunar rover and has the people to drive two kinds on the lunar rover vehicle, the unmanned lunar rover is made up of wheel undercarriage and instrument compartment, unite power supply with solar cell and storage battery, travelling of this class lunar rover vehicle is by the ground remote control instruction control; Someone drives the lunar rover vehicle is to be driven in the car of walking on the moonscape by the cosmonaut, be mainly used in the action radius that enlarges the cosmonaut and reduce physical demands, can deposit rock and soil sampling that the cosmonaut gathers at any time, each wheel of this class lunar rover vehicle is respectively by an engine drive, provide power by storage battery, tire still can keep elasticity at low temperatures, and cosmonaut's bar handle is driven the lunar rover vehicle, can be forward, backward, turn and climbing.With respect to the unmanned lunar rover, someone drives the deployable work of the lunar rover vehicle and seems more extensive, performance is also more excellent, but carry out in the work of moonscape owing to relate to personnel, each side requires also corresponding raising, training from personnel, the expenditure of cost, the safety performance all angles, the capital faces no small pressure, also have many uncertain unknown situation in addition, so the unpiloted lunar rover vehicle is in fact also adopted widely, though and present unmanned lunar rover in these areas relatively the someone drive the lunar rover vehicle some advantages arranged, if but in the detection driving process of practical operation, suffer from situations such as with a varied topography, the difficult processing of meeting, common way is to get around obstacle, if the obstacle that runs into is enough big, even walk around smoothly, information that it collects and data also might not be very definite.
The utility model content
Technical problem to be solved in the utility model is to overcome existing unmanned lunar rover's above shortcomings, a kind of solar power lunar rover vehicle of the intricately condition that can tackle in the data acquisition flexibly to be run into is provided, and its technical matters to be solved can be implemented by the following technical programs.
A kind of solar power lunar rover vehicle, comprise that main control centre module, communication feedway, energy resource supply module, visual identification module, sampling drilling module, sample deposit the cabin and hang advance system, this lunar rover vehicle also comprises aircraft, on the described aircraft detector is installed, described lunar rover vehicle is provided with the aircraft stop device of parking this aircraft.
Further, be provided with the control module of the described aircraft operation of control in the described communication feedway.Described energy resource supply module comprises the solar panel that is arranged on lunar rover vehicle surface and the energy storage cabin that can store the collected energy of solar panel and reserve energy cabin.
As further improvement, described sampling drilling module comprises sampling mechanical arm and rock stratum drilling rig.Described aircraft stop device is the aircraft stop cabin of being located at lunar rover vehicle upper end flat-bed aircraft docking station and being located at cabin in the lunar rover vehicle.
The solar power lunar rover vehicle of this technical scheme of sampling, can be implemented under complex environment and the unpredictable moon exploration situation, with less cost and lower cost, by introducing the purpose that the flight detector reaches accurate measurement and analyzes data and sample, the some shortcomings of also having avoided the participation owing to the cosmonaut to bring simultaneously.
Description of drawings
Below in conjunction with accompanying drawing the specific embodiment of the present utility model being done one describes in detail.
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is the upward view of the lunar rover vehicle described in the utility model.
Among the figure: 1, main control centre 2, communication launch tower 3, solar panel
4, three dimensional vision system 5, sampling mechanical arm (hand) 6, rock stratum drilling rig
7, sample is deposited cabin 8, aircraft 9, aircraft docking station
10, energy storage cabin 11, reserve energy cabin 12, independent suspension advance system
The specific embodiment
Solar power lunar rover vehicle as depicted in figs. 1 and 2, comprise main control centre 1, communication launch tower 2, solar panel 3, three dimensional vision system 4, sampling mechanical arm (hand) 5, rock stratum drilling rig 6, as the sample of assay laboratory deposit cabin 7, aircraft 8, aircraft docking station 9, energy storage cabin 10, reserve energy cabin 11, two take turns one group eight take turns functional component such as independent suspension advance system 12.
The three dimensional vision system 4 that several places of the lunar rover vehicle are provided with respectively is as the visual identification module on the lunar rover vehicle, also play simultaneously the effect of illumination, it is by fully-directional visual system conduct multiobject real-time monitoring greatly within sweep of the eye, obtain the environment visual information of lunar rover vehicle periphery by this system, the vision system that is positioned at lunar rover vehicle top has been set up key lighting equipment, can and coordinate the main travel track of the lunar rover vehicle as the key lighting in the lunar rover vehicle traveling process, and the vision system that is positioned at lunar rover vehicle bottom front end is used to coordinate the mechanical arm hand to grasping the action of object, make it to gather accurately sample, also set up the sampling light equipment simultaneously and can under dark surrounds, provide illumination.
Be positioned at the sampling mechanical arm (hand) 5 of lunar rover vehicle front end top, adopt the scalable mechanical arm of three degree of freedom, can stretch the orientation that arrives appointment flexibly.The mechanical arm front end is a manipulator with four fingers, each finger has three joints, at each finger top setting pressure sensor, grip that can actv. control manipulator is got rid of the obstacle that runs in the traveling process by accepting the instruction that main control centre 1 sends.
Set rock stratum drilling rig 6 can realize the moon face of land is carried out the probing of certain depth in lunar rover vehicle bottom, and sample, analyze, and the sample gathered and deposit data deposited cabin 7 at the sample as the assay laboratory that is adjacent, this freight space is on the limit of mechanical arm hand 5, be used to deposit the sample that collects, and the sample that collects analyzed, the data of analyzing gained are sent back earth control center again.
The aircraft 8 that all kinds of detectors are installed can be explored the region that some lunar rover vehiclies can't arrive, also can carry out the near-earth aerological ascent to a certain area, thereby the introducing of this aircraft has substituted a few thing that the cosmonaut finished to a certain extent, and relatively the cosmonaut it is stronger to environment requirement and adaptive capacity.Stop for aircraft 8, this lunar rover vehicle also is provided with aircraft specially and stops the cabin, aircraft can be taken in the aircraft in the interior cabin that is arranged on lunar rover vehicle from the deck and be stopped the cabin, also aircraft 8 can be parked in and be located on the lunar rover vehicle upper end flat-bed aircraft docking station 9.
The suspension advance system of the lunar rover vehicle is eight to take turns (two take turns one group) independent suspension advance system 12, because moonscape geographical environment complexity, it is especially important that the manoevreability of lunar rover vehicle shows, and adopted the bigger artillery wheel of face area, and to take turns with two be one group mode, constitutes a relatively independent wheel.Each group wheel has separately independently suspension, and according to the road conditions of moonscape, four group wheels can lead to micro computer and carry out co-operative control, can tackle the environment of more complicated.
When lunar rover vehicle after moonscape lands, assignment instructions is sent in the ground control center, vehicle-borne master controller begins according to default program run after receiving instruction.Utilize the intelligent transducer on the lunar rover vehicle independently to travel to the destination, lunar rover vehicle is before setting out in the destination, emit vehicle-borne small aircraft 8 earlier, aircraft can be taken subaerial photo of getting a bird's eye view in the high-altitude, after photo is passed lunar rover vehicle main control centre 1 back, pass the ground control center again back, the course of lunar rover vehicle is formulated by the analysis of comparison film in the ground control center, finally instruction is passed back lunar rover vehicle again.If when lunar rover vehicle runs into the zone that can't go to such as valley, meteorite crater, mountain range, cavern etc., can emit small aircraft 8 too and go to exploration, and in time pass relevant information back.Three dimensional vision system 4 sends back vision signal to earth control center, and video signal delay is about 1.5 seconds.Lunar rover vehicle can change the ground control center into and carry out manual manipulation when advancing to more regional of obstacle.The sampling mechanical arm (hand) 5 in lunar rover vehicle the place ahead can be moved some obstacles on the course.When lunar rover vehicle advances to the destination, the rock stratum drilling rig 6 of car body below stretches out, carry out the probing sampling work of moonscape rock stratum, put into the sample storage cabin 7 of lunar rover vehicle after manipulator grasps the sample rock that gathers, further analyze and analysis result is sent back the ground control center.By the compound sensor on the lunar rover vehicle, the element that can measure magnetic field, the Lunar surface temperature of different periods, the lunar rock of the moon constitutes, gravitational field or the like basic physical data and chemical data.
This lunar rover vehicle is with respect to existing unmanned lunar rover and have the people to drive the lunar rover vehicle, under unmanned situation, effectively reduce the operation of the lunar rover vehicle and the requirement of working environment, and realized function widely by introducing the flight detector, will bring into play bigger reality and positive role for the exploration of the moon.
Claims (5)
1. solar power lunar rover vehicle, comprise that main control centre module, communication feedway, energy resource supply module, visual identification module, sampling drilling module, sample deposit the cabin and hang advance system, it is characterized in that: this lunar rover vehicle also comprises aircraft, on the described aircraft detector is installed, described lunar rover vehicle is provided with the aircraft stop device of parking this aircraft.
2. solar power lunar rover vehicle according to claim 1 is characterized in that: the control module that is provided with the described aircraft operation of control in the described communication feedway.
3. solar power lunar rover vehicle according to claim 1 is characterized in that: described energy resource supply module comprises the solar panel that is arranged on lunar rover vehicle surface and the energy storage cabin that can store the collected energy of solar panel and reserve energy cabin.
4. solar power lunar rover vehicle according to claim 1 is characterized in that: described sampling drilling module comprises sampling mechanical arm and rock stratum drilling rig.
5. solar power lunar rover vehicle according to claim 1 is characterized in that: described aircraft stop device is the aircraft stop cabin of being located at lunar rover vehicle upper end flat-bed aircraft docking station and being located at cabin in the lunar rover vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200681287U CN201040587Y (en) | 2007-03-23 | 2007-03-23 | Solar energy lunar excursion vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200681287U CN201040587Y (en) | 2007-03-23 | 2007-03-23 | Solar energy lunar excursion vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201040587Y true CN201040587Y (en) | 2008-03-26 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007200681287U Expired - Fee Related CN201040587Y (en) | 2007-03-23 | 2007-03-23 | Solar energy lunar excursion vehicle |
Country Status (1)
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|---|---|
| CN (1) | CN201040587Y (en) |
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102187290A (en) * | 2008-10-13 | 2011-09-14 | Dcns公司 | Method and system for controlling the automatic landing/take-off of a drone on or from a circular landing grid of a platform, in particular a naval platform |
| CN102189546A (en) * | 2011-05-26 | 2011-09-21 | 江苏科技大学 | Multifunctional mechanical arm for planet exploration vehicle |
| CN102530266A (en) * | 2012-02-29 | 2012-07-04 | 大连理工大学 | Vehicle body device for lunar landing vehicle |
| CN101704416B (en) * | 2009-11-20 | 2013-06-05 | 河南科技大学 | Lunar vehicle |
| CN103170987A (en) * | 2011-12-21 | 2013-06-26 | 中国科学院沈阳自动化研究所 | Planet surface mechanical arm sampling device |
| CN103488173A (en) * | 2013-09-09 | 2014-01-01 | 上海电控研究所 | Multi-terrain intelligent mobile platform and control method thereof |
| CN104108475A (en) * | 2014-06-30 | 2014-10-22 | 上海宇航系统工程研究所 | Multifunctional manned lunar vehicle |
| WO2015057832A1 (en) * | 2013-10-15 | 2015-04-23 | Elwha Llc | Motor vehicle with captive aircraft |
| CN106198100A (en) * | 2016-08-01 | 2016-12-07 | 昆明理工大学 | A kind of multi-joint lunar surface material sniffing robot |
| CN106444751A (en) * | 2016-09-17 | 2017-02-22 | 哈尔滨理工大学 | Movement control system for manned moon rover |
| CN108639380A (en) * | 2018-03-29 | 2018-10-12 | 北京空间技术研制试验中心 | Lunar surface sniffing robot |
| CN109305390A (en) * | 2018-09-27 | 2019-02-05 | 哈尔滨工业大学 | Anchor pull-type star catalogue mobile device and its moving method |
| CN110014434A (en) * | 2019-04-19 | 2019-07-16 | 昆明理工大学 | A kind of lunar base construction robot |
| CN111015620A (en) * | 2019-11-25 | 2020-04-17 | 北京空间飞行器总体设计部 | Flying and walking integrated robot suitable for weak gravity star-watch detection |
| CN111891237A (en) * | 2020-08-19 | 2020-11-06 | 大连理工大学 | All-terrain scientific investigation vehicle |
| CN113146675A (en) * | 2021-02-25 | 2021-07-23 | 北京空间飞行器总体设计部 | Lunar surface sampling mechanical arm joint |
-
2007
- 2007-03-23 CN CNU2007200681287U patent/CN201040587Y/en not_active Expired - Fee Related
Cited By (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102187290B (en) * | 2008-10-13 | 2013-08-14 | Dcns公司 | Method and system for controlling the automatic landing/take-off of a drone on or from a circular landing grid of a platform, in particular a naval platform |
| CN102187290A (en) * | 2008-10-13 | 2011-09-14 | Dcns公司 | Method and system for controlling the automatic landing/take-off of a drone on or from a circular landing grid of a platform, in particular a naval platform |
| CN101704416B (en) * | 2009-11-20 | 2013-06-05 | 河南科技大学 | Lunar vehicle |
| CN102189546A (en) * | 2011-05-26 | 2011-09-21 | 江苏科技大学 | Multifunctional mechanical arm for planet exploration vehicle |
| CN103170987B (en) * | 2011-12-21 | 2015-06-03 | 中国科学院沈阳自动化研究所 | Planet surface mechanical arm sampling device |
| CN103170987A (en) * | 2011-12-21 | 2013-06-26 | 中国科学院沈阳自动化研究所 | Planet surface mechanical arm sampling device |
| CN102530266A (en) * | 2012-02-29 | 2012-07-04 | 大连理工大学 | Vehicle body device for lunar landing vehicle |
| CN102530266B (en) * | 2012-02-29 | 2013-12-25 | 大连理工大学 | Vehicle body device for lunar landing vehicle |
| CN103488173A (en) * | 2013-09-09 | 2014-01-01 | 上海电控研究所 | Multi-terrain intelligent mobile platform and control method thereof |
| CN103488173B (en) * | 2013-09-09 | 2016-08-17 | 上海电控研究所 | Many landform intelligent family moving platform and control method thereof |
| US10112710B2 (en) | 2013-10-15 | 2018-10-30 | Elwha Llc | Motor vehicle with captive aircraft |
| EP3057857A4 (en) * | 2013-10-15 | 2017-07-26 | Elwha, Llc | Motor vehicle with captive aircraft |
| US9969490B2 (en) | 2013-10-15 | 2018-05-15 | Elwha Llc | Motor vehicle with captive aircraft |
| WO2015057832A1 (en) * | 2013-10-15 | 2015-04-23 | Elwha Llc | Motor vehicle with captive aircraft |
| CN104108475A (en) * | 2014-06-30 | 2014-10-22 | 上海宇航系统工程研究所 | Multifunctional manned lunar vehicle |
| CN106198100A (en) * | 2016-08-01 | 2016-12-07 | 昆明理工大学 | A kind of multi-joint lunar surface material sniffing robot |
| CN106198100B (en) * | 2016-08-01 | 2018-10-02 | 昆明理工大学 | A kind of multi-joint lunar surface material sniffing robot |
| CN106444751A (en) * | 2016-09-17 | 2017-02-22 | 哈尔滨理工大学 | Movement control system for manned moon rover |
| CN108639380A (en) * | 2018-03-29 | 2018-10-12 | 北京空间技术研制试验中心 | Lunar surface sniffing robot |
| CN109305390A (en) * | 2018-09-27 | 2019-02-05 | 哈尔滨工业大学 | Anchor pull-type star catalogue mobile device and its moving method |
| CN109305390B (en) * | 2018-09-27 | 2020-07-14 | 哈尔滨工业大学 | Anchoring and dragging type star catalogue moving device and moving method thereof |
| CN110014434A (en) * | 2019-04-19 | 2019-07-16 | 昆明理工大学 | A kind of lunar base construction robot |
| CN111015620A (en) * | 2019-11-25 | 2020-04-17 | 北京空间飞行器总体设计部 | Flying and walking integrated robot suitable for weak gravity star-watch detection |
| CN111015620B (en) * | 2019-11-25 | 2021-09-03 | 北京空间飞行器总体设计部 | Flying and walking integrated robot suitable for weak gravity star-watch detection |
| CN111891237A (en) * | 2020-08-19 | 2020-11-06 | 大连理工大学 | All-terrain scientific investigation vehicle |
| CN113146675A (en) * | 2021-02-25 | 2021-07-23 | 北京空间飞行器总体设计部 | Lunar surface sampling mechanical arm joint |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20080326 |