CN108394571A - The test platform and measurement method of flexible surface adherency movement under simulated microgravity - Google Patents

The test platform and measurement method of flexible surface adherency movement under simulated microgravity Download PDF

Info

Publication number
CN108394571A
CN108394571A CN201810118313.5A CN201810118313A CN108394571A CN 108394571 A CN108394571 A CN 108394571A CN 201810118313 A CN201810118313 A CN 201810118313A CN 108394571 A CN108394571 A CN 108394571A
Authority
CN
China
Prior art keywords
flexible surface
speed camera
adherency
strain gage
resistance strain
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201810118313.5A
Other languages
Chinese (zh)
Other versions
CN108394571B (en
Inventor
俞志伟
石叶
陶洁莲
罗奥
谢家兴
王周义
戴振东
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nanjing University of Aeronautics and Astronautics
Original Assignee
Nanjing University of Aeronautics and Astronautics
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nanjing University of Aeronautics and Astronautics filed Critical Nanjing University of Aeronautics and Astronautics
Priority to CN201810118313.5A priority Critical patent/CN108394571B/en
Publication of CN108394571A publication Critical patent/CN108394571A/en
Application granted granted Critical
Publication of CN108394571B publication Critical patent/CN108394571B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G7/00Simulating cosmonautic conditions, e.g. for conditioning crews

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manipulator (AREA)
  • Toys (AREA)

Abstract

The test platform and measurement method of flexible surface adherency movement, belong to robot field under simulated microgravity.The flexible surface of the system(11)Test contact reverse side uniformly post the resistance strain gage (9) in array distribution.The bending of flexible surface (11) can lead to resistance strain gage (9) resistance variations, resistance strain gage (9) increased resistance value, which is acquired, by sensing data acquisition system measures flexible surface (11) bending curvature indirectly, bond material flexible surface (11) elasticity modulus measures the moment of flexure and power of flexible surface at this (11) indirectly, by determining resistance strain gage (9) in flexible surface (11) plane distribution position, you can acquire the moment of flexure and force value everywhere in flexible surface.It is convenient that the configuration of the present invention is simple, motion principle are clear, movement is realized.

Description

The test platform and measurement method of flexible surface adherency movement under simulated microgravity
Technical field
The invention belongs to robot technology application fields, and in particular to flexible surface adherency movement under a kind of simulated microgravity Test platform and measurement method.
Background technology
Since the former Soviet Union in 1956 emits first artificial satellite, space flight skill is benefited from the life of the mankind more and more The development of art.Space technology profoundly changes the life of the mankind, represents national science and technology strength and overall national strength, simul relation To national economic interest and national defense safety, the space safety for also affecting countries in the world is seen.The Disciplinary Frontiers of space technology include In-orbit service, survey of deep space etc., wherein in-orbit service refer to be completed in space to spacecraft event by people, robot or both collaboration The spatial operation that barrier repairs, lengthens the life, Mission Capability is promoted is mainly included in rail assembly, In-flight measurement maintenance and logistics branch Hold equal service roles.Robot for space applied to On-orbit servicing is the project in current robot research field forward position the most One of.
Therefore, ground simulation microgravity environment carries out robot for space ground experiment research early period, exists to robot for space Rail practical application is of great significance and practical value.It is especially following that robot is adhered to using space, such as satellite sun sail, It is important replacing astronaut to complete when the surface adhesions such as film antenna, hull cell battle array, outer surface flexible cover sheet move operation In-orbit maintenance task in terms of play and play an important roll.
Space microgravity environment is generally simulated using suspension method, Bubble-floating Method, water float glass process as far as possible both at home and abroad.It is directed at present Analog form of the sufficient formula adherency robot under microgravity environment, mainly offsets the shadow of gravity by balloon suspension mode It rings, carries out the observation robot motion on the horizontal plane of hard ground(National inventing patent:Dai Zhendong, Wang Zhongyuan, Sun Gongxun Experimental system and ground experiment method number of patent application of the gecko-emulated robot under microgravity environment: CN201510273695.5).Applicant was once directed to imitative gecko robot for space posture in the flight course under microgravity and regulated and controled It is studied with the problem in science for moment adherency of landing, it is proposed that the relevant experimental system and method flight attitude regulation and control and landed, (National inventing patent:Yu Zhiwei, Dai Zhendong, Yang Bin, Ji Aihong, Wang Zhongyuan imitate the regulation and control of gecko robot for space posture with Land experimental system and method number of patent application:CN201510096242.X), but do not propose that really sufficient formula is viscous on flexible surface The test method of attached movement.
So far, under ground simulation microgravity environment in flexible surface (such as satellite sun sail, film antenna, thin Film battery battle array, satellite external surface flexible cover sheet) on sufficient formula adherency exercise test system not yet report.
Invention content
The purpose of the present invention is to provide one kind ground can under stimulated microgravity sufficient formula adherency movement in flexible table The mechanics in face and performance testing system.
The test platform of flexible surface adherency movement and measurement method, feature exist under a kind of simulated microgravity In:
The main structure of system includes platform base, support scale bar and roof supporting, and wherein platform base is horizontal positioned, support Scale bar is perpendicularly fixed on platform base, and roof supporting is horizontally arranged and is fixed on support scale bar top;Support base one end It fixes with roof supporting, is connected through the hinge between support base and flexible surface, angular transducer is coaxially fixed with hinge;It is flexible The test contact reverse side on surface uniformly posts the resistance strain gage in array distribution, and micro-inertial navigation module is fixed on flexible surface Bottom end;Micro-inertial navigation module, resistance strain gage, angular transducer pass through data/address bus with sensing data acquisition system respectively Connection;Sensing data acquisition system is communicated with computer control terminal by data/address bus;X is to sliding shoe top and roof supporting Between there is prismatic pair in X direction;X secures I fixed pulleys and II fixed pulleys to sliding shoe bottom end, I fixed pulleys and II fixed pulleys keep identical height level;X is fixed on X on tripod to high-speed camera, and X is to high-speed camera along X-axis It is directed at flexible surface;Y-direction high-speed camera is fixed on roof supporting, and Y-direction high-speed camera is perpendicular along Y-axis alignment flexible surface Straight sided;Z-direction high-speed camera is fixed on Z-direction tripod, and Z-direction high-speed camera is directed at flexible surface horizontal side along Z axis; X passes through data/address bus phase with computer control terminal respectively to high-speed camera, Y-direction high-speed camera and Z-direction high-speed camera Even;Cord one end connects legged type robot main body, and the cord other end coils through II fixed pulleys and I fixed pulleys successively, even Connect mass;Legged type robot main body is equipped with robot wireless communication module;Computer control terminal and host computer channel radio It interrogates module to be connected, host computer wireless communication module and robot wireless communication module holding wireless telecommunications;Legged type robot main body Tail portion connects tail;Light source is fixed on roof supporting bottom surface, and direction is directed at flexible surface and legged type robot main body.With such It pushes away, cord one end connects shoulder strap, and the cord other end coils through II fixed pulleys and I fixed pulleys successively, connects mass;The back of the body Band can be mounted on four-footed adherency animal, carry out mechanics and performance testing that animal is adhered to about four-footed.
The measurement method of flexible surface adherency movement under the simulated microgravity, it is characterised in that including following procedure:
Step 1, the four-footed adherency animal (such as gecko-emulated robot or biological gecko) by legged type robot main body or installation shoulder strap Be suspended on cord one end, the cord other end ties up to mass, mass and testee are equal in weight, constitute simulated microgravity Environmental condition;
Step 2 makes X be directed at testee and its area of observation coverage to high-speed camera, Y-direction high-speed camera, Z-direction high-speed camera Domain, by computer control terminal high-speed record testee in X, Y and Z-motion video image information;
Step 3, computer control terminal transmit a signal to robot wireless communication module by host computer wireless communication module, control The forms of motion of the four limbs and tail of legged type robot main body processed;
Uniformly distributed identical resistance strain gage, forms m n array above step 4, flexible surface, and the bending of flexible surface can cause Resistance strain gage resistance variations obtain resistance strain gage increased resistance value and flexible surface using traditional experimental calibration method Bending curvature relationship, therefore resistance strain gage increased resistance value is acquired by sensing data acquisition system and measures flexible surface indirectly Bending curvature, while it being based on mechanics of materials model and calculation formula, it is calculated indirectly in conjunction with the elasticity modulus of compliant surface material The moment of flexure and power of flexible surface at this, by determining resistance strain gage in flexible surface plane distribution position, you can acquire soft Moment of flexure and force value everywhere in property surface;
Step 5 can cause flexible surface to swing since adherency moves, and the setting angle sensor at hinge passes through sensing data Acquisition system can detect flexible surface angle of oscillation angle value;The micro-inertial navigation module of flexible surface bottom end obtains swing process simultaneously In acceleration value and terminal angle angle, by sensing data acquisition system acquire after, be computer controlled terminal reading;
Step 6, by X to high-speed camera, Y-direction high-speed camera, Z-direction high-speed camera, computer control terminal and sensing Data collecting system, have recorded legged type robot main body or four-footed adherency animal multi-motion gait and flexible surface moment of flexure and Power, oscillating acceleration and swing angle can carry out the adherency exercise test under template microgravity;
Step 7, the moment of flexure and power of the flexible surface obtained by sensing data acquisition system, oscillating acceleration and swing angle are made For motion-sensing feedback data, corresponding movement gait data is taken by computer control terminal, regulates and controls legged type robot master The quadruped locomotion form and tail of body swing mode, reach the control targe for keeping flexible surface chatter amplitude small.
The test platform and measurement method of flexible surface adherency movement, can be applied to observation four under the simulated microgravity The image recording and flexible surface moment of flexure and power, oscillating acceleration and pendulum of forms of motion of the foot adherency animal under simulated microgravity Dynamic angular relationship;Flexible surface moment of flexure and power, oscillating acceleration and the swing angle feedback that may be based on acquisition, to regulate and control sufficient formula The quadruped locomotion form and tail of robot body swing mode, under simulated microgravity to reach flexible surface chatter amplitude small Control targe, contribute to future space adherency robot flexible surface (such as satellite sun sail, film day under microgravity environment Line, hull cell battle array, satellite external surface flexible cover sheet) on adherency locomotive regulation technological reserve and ground simulation demonstration.
The present invention has the following advantages compared with prior art:
1, the present invention adheres to performance test demand when moving for microgravity environment down space legged type robot in flexible surface, Flexible surface of the suspension with more heat transfer agent devices is dexterously devised, testee is balanced using suspended counterweight mode, is adopted Synchronized tracking, acquisition and the processing data that mechanics and behavior are carried out with 3 d image and video acquisition device, have been filled up in the field The blank of test method.
2, it is convenient that structure of the invention is simple, motion principle is clear, movement is realized, meets space legged type robot and four-footed Performance evaluation requirement of the animal when flexible surface is walked is adhered to, the space foot formula machine under ground simulation microgravity environment is improved Experiment test performance of the device people in flexible surface adherency movement.
3, the present invention has recorded the video image of quadruped robot and four-footed adherency animal, flexible surface swing angle letter Number, flexible surface deformation and by force signal, flexible surface end acceleration and attitude signal, be that quadruped robot and four-footed adhere to The further experiment analysis of animal provides sufficient sensing data, is to be adhered in flexible surface under robot for space microgravity environment Movenent performance test provides beneficial way and good experimental facilities.
For this purpose, we bioadhesion movement it is bionical on the basis of, carry out ground simulation microgravity environment under, in flexible table Four-footed adherency exercise testing is carried out on face and four-footed adheres to animal(Such as gecko)Movement mechanism research, at home and abroad belong to prediction Journal of Sex Research, the test platform of flexible surface adherency movement will have certain innovation with measurement method under the simulated microgravity of design Property, the mechanics of the four-footed adherency movement under the ground simulation microgravity environment of development on flexible surface and performance testing research, The research of its related scientific issues is estimated can to obtain achievement leading in the world.
Description of the drawings
Fig. 1 is the test platform block diagram I of flexible surface adherency movement under simulated microgravity of the present invention;
Fig. 2 is the test platform block diagram II of flexible surface adherency movement under simulated microgravity of the present invention.
Above-mentioned figure label title:1, X is to high-speed camera, 2, X to tripod, 3, Z-direction high-speed camera, 4, Z-direction three Tripod, 5, host computer wireless communication module, 6, computer control terminal, 7, sensing data acquisition system, 8, micro-inertial navigation mould Block, 9, resistance strain gage, 10, support scale bar, 11, flexible surface, 12, hinge, 13, angular transducer, 14, support base, 15, Y-direction high-speed camera, 16, roof supporting, 17, light source, 18, X to sliding shoe, 19, I fixed pulleys, 20, II fixed pulleys, 21, Mass, 22, cord, 23, legged type robot main body, 24, robot wireless communication module, 25, tail, 26, platform base, 27, shoulder strap, 28, four-footed adhere to animal.
X is to for flexible surface normal orientation in figure;Y-direction is for gravity direction;Z-direction is for horizontal direction.
Specific implementation mode
Invention is further described in detail in the following with reference to the drawings and specific embodiments:
In conjunction with Fig. 1, the present embodiment is a kind of test platform of flexible surface adherency movement under simulated microgravity, including X at a high speed Video camera 1, X are whole to tripod 2, Z-direction high-speed camera 3, Z-direction tripod 4, host computer wireless communication module 5, computer control End 6, sensing data acquisition system 7, micro-inertial navigation module 8, resistance strain gage 9, support scale bar 10, flexible surface 11, hinge Chain 12, angular transducer 13, support base 14, Y-direction high-speed camera 15, roof supporting 16, light source 17, X are to sliding shoe 18, I Fixed pulley 19, II fixed pulleys 20, mass 21, cord 22, legged type robot main body 23, robot wireless communication module 24, Tail 25, platform base 26 form.
As shown in Figure 1, the test platform that flexible surface adherency moves under a kind of simulated microgravity, feature exist In:The main structure of system includes that platform base 26, support scale bar 10 and roof supporting 16, wherein 26 level of platform base are put It sets, support scale bar 10 is perpendicularly fixed on platform base 26, and roof supporting 16 is horizontal positioned and is fixed on support scale bar 10 Top;14 one end of support base is fixed with roof supporting 16, is connected by hinge 12 between support base 14 and flexible surface 11, angle Sensor 13 is coaxial fixed with hinge 12;The test contact reverse side of flexible surface 11 uniformly posts the resistance-strain in array distribution Piece 9, micro-inertial navigation module 8 are fixed on the bottom end of flexible surface 11;Micro-inertial navigation module 8, resistance strain gage 9, angle pass Sensor 13 is connect with sensing data acquisition system 7 by data/address bus respectively;Sensing data acquisition system 7 and computer control are whole End 6 is communicated by data/address bus;X is to having prismatic pair in X direction between 18 top of sliding shoe and roof supporting 16;X is to cunning 18 bottom end of motion block secures I fixed pulleys 19 and II fixed pulleys 20, and I fixed pulleys 19 and II fixed pulleys 20 keep identical water Flat height;X is fixed on X on tripod 2 to high-speed camera 1, and X is directed at flexible surface 11 to high-speed camera 1 along X-axis; Y It is fixed on roof supporting 16 to high-speed camera 14, Y-direction high-speed camera 14 is along 11 vertical side of Y-axis alignment flexible surface;Z It is fixed on Z-direction tripod 4 to high-speed camera 3, Z-direction high-speed camera 3 is directed at 11 horizontal side of flexible surface along Z axis;X to High-speed camera 1, Y-direction high-speed camera 14 and Z-direction high-speed camera 3 pass through data/address bus with computer control terminal 6 respectively It is connected;22 one end of cord connects legged type robot main body 23, and 22 other end of cord coils through II fixed pulleys 20 and No. I successively Fixed pulley 19 connects mass 21;Legged type robot main body 23 is equipped with robot wireless communication module 24;Computer controls Terminal 6 is connected with host computer wireless communication module 5, and host computer wireless communication module 5 is kept with robot wireless communication module 24 Wireless telecommunications;23 tail portion of legged type robot main body connects tail 25;Light source 17 is fixed on 16 bottom surface of roof supporting, and direction alignment is soft Property surface 11 and legged type robot main body 23.
In conjunction with Fig. 2, the present embodiment be a kind of simulated microgravity under flexible surface adherency movement test platform, including X to High-speed camera 1, X are to tripod 2, Z-direction high-speed camera 3, Z-direction tripod 4, host computer wireless communication module 5, computer control Terminal 6 processed, sensing data acquisition system 7, micro-inertial navigation module 8, resistance strain gage 9, support scale bar 10, flexible surface 11, hinge 12, angular transducer 13, support base 14, Y-direction high-speed camera 15, roof supporting 16, light source 17, X are to sliding shoe 18, I fixed pulleys 19, II fixed pulleys 20, mass 21, cord 22, platform base 26, shoulder strap 27, four-footed adhere to animal 28 Composition.
As shown in Fig. 2, flexible surface adherency moves under a kind of simulated microgravity test platform and measurement method, It is characterized in that:The main structure of system includes platform base 26, support scale bar 10 and roof supporting 16, wherein platform base 26 is horizontal positioned, and support scale bar 10 is perpendicularly fixed on platform base 26, and roof supporting 16 is horizontal positioned and is fixed on support 10 top of scale bar;14 one end of support base is fixed with roof supporting 16, passes through hinge 12 between support base 14 and flexible surface 11 Connection, angular transducer 13 are coaxial fixed with hinge 12;The test contact reverse side of flexible surface 11 is uniformly posted in array distribution Resistance strain gage 9, micro-inertial navigation module 8 is fixed on the bottom end of flexible surface 11;Micro-inertial navigation module 8, resistance-strain Piece 9, angular transducer 13 are connect with sensing data acquisition system 7 by data/address bus respectively;Sensing data acquisition system 7 and meter Calculation machine control terminal 6 is communicated by data/address bus;X is to having shifting in X direction between 18 top of sliding shoe and roof supporting 16 Dynamic pair;X secures I fixed pulleys 19 and II fixed pulleys 20, I fixed pulleys 19 and II fixed pulleys 20 to 18 bottom end of sliding shoe Keep identical height level;X is fixed on X on tripod 2 to high-speed camera 1, and X is to high-speed camera 1 along X-axis to quasi-flexible Surface 11;Y-direction high-speed camera 14 is fixed on roof supporting 16, and Y-direction high-speed camera 14 is directed at flexible surface 11 along Y-axis Vertical side;Z-direction high-speed camera 3 is fixed on Z-direction tripod 4, and Z-direction high-speed camera 3 is directed at 11 water of flexible surface along Z axis Plane side;X is logical with computer control terminal 6 respectively to high-speed camera 1, Y-direction high-speed camera 14 and Z-direction high-speed camera 3 Data/address bus is crossed to be connected;22 one end of cord connects shoulder strap 27, and 22 other end of cord coils through II fixed pulleys 20 and No. I successively Fixed pulley 19 connects mass 21;Shoulder strap 27 is mounted on four-footed adherency animal 28;Light source 17 is fixed on 16 bottom of roof supporting Face, direction is directed at flexible surface 11 and four-footed adheres to animal 28.
The measurement method of flexible surface adherency movement under the simulated microgravity, it is characterised in that including following procedure:
The four-footed of legged type robot main body 23 or installation shoulder strap 27 is adhered to animal 28 (such as gecko-emulated robot or life by step 1 Object gecko) be suspended on 22 one end of cord, 22 other end of cord ties up to mass 21, mass 21 and testee are equal in weight, Constitute stimulated microgravity condition;
Step 2 makes X be directed at testee and its sight to high-speed camera 1, Y-direction high-speed camera 14, Z-direction high-speed camera 3 Region is surveyed, by 6 high-speed record testee of computer control terminal in X, Y and Z-motion video image information;
Step 3, computer control terminal 6 can control the four limbs of legged type robot main body 23 by host computer wireless communication module 5 With the forms of motion of tail 25;
Uniformly distributed identical resistance strain gage 9 has above for step 4, flexible surface 11(m×n)Several, the bending of flexible surface 11 Can lead to 9 resistance variations of resistance strain gage, using traditional experimental calibration method, obtain 9 increased resistance value of resistance strain gage and 11 bending curvature relationship of flexible surface, thus by sensing data acquisition system 7 acquire resistance strain gage 9 increased resistance value can between It connects and measures 11 bending curvature of flexible surface, while being based on mechanics of materials model and calculation formula, in conjunction with 11 material of flexible surface Elasticity modulus can calculate the moment of flexure and power of flexible surface 11 at this indirectly, by determining resistance strain gage 9 in flexible table 11 plane distribution position of face, you can acquire moment of flexure and force value everywhere in flexible surface 11;
Step 5 can cause flexible surface 11 to swing since adherency moves, and the setting angle sensor 13 at hinge 12 passes through biography Sense data collecting system 7 can detect 11 angle of oscillation angle value of flexible surface;The micro-inertial navigation module 8 of 11 bottom end of flexible surface simultaneously The acceleration value and terminal angle angle in swing process are obtained, after being acquired by sensing data acquisition system 7, by computer control Terminal 6 processed is read;
Step 6, by X to high-speed camera 1, Y-direction high-speed camera 14, Z-direction high-speed camera 3,6 and of computer control terminal Sensing data acquisition system 7 has recorded legged type robot main body 23 or four-footed adherency 28 multi-motion gait of animal and flexible table The moment of flexure and power in face 11, oscillating acceleration and swing angle can carry out the adherency exercise test under template microgravity;
Step 7, the moment of flexure and power of flexible surface 11 obtained by sensing data acquisition system 7, oscillating acceleration and angle of oscillation Degree is used as motion-sensing feedback data, and corresponding movement gait data is taken by computer control terminal 6, regulates and controls sufficient formula machine The quadruped locomotion form and tail 25 of human agent 23 swings mode, reaches the control mesh for keeping 11 chatter amplitude of flexible surface small Mark.
The test platform and measurement method of flexible surface adherency movement, can be applied to observation four under the simulated microgravity The image recording and 11 moment of flexure of flexible surface and power, oscillating acceleration of forms of motion of the foot adherency animal 28 under simulated microgravity With swing angle relationship;11 moment of flexure of flexible surface and power, oscillating acceleration and the swing angle feedback that may be based on acquisition, to adjust The quadruped locomotion form and tail 25 for controlling legged type robot main body 23 swing mode, reach flexible surface under simulated microgravity The small control targe of 11 chatter amplitudes contributes to future space adherency robot flexible surface (such as satellite under microgravity environment Solar sail, film antenna, hull cell battle array, satellite external surface flexible cover sheet) on adherency locomotive regulation technological reserve and ground Face simulation demo.

Claims (4)

1. the test platform of flexible surface adherency movement under a kind of simulated microgravity, to legged type robot or four-footed adhere to animal into Row experiment, it is characterised in that:
The test platform includes platform base(26), support scale bar(10)With roof supporting (16);Wherein platform base (26) Horizontal positioned, support scale bar (10) is perpendicularly fixed on platform base (26), and roof supporting (16) is horizontal positioned and is fixed on Support scale bar (10) top;
The test platform further includes support base (14) and flexible surface(11);Wherein support base (14) one end and roof supporting (16) Fixed, support base (14) other end is connected through the hinge with flexible surface (11) upper end, and hinged (12) axis and roof supporting (16) parallel, flexible surface (11) lower end is free end;Above-mentioned hinge (12) is co-axially mounted angular transducer (13);Above-mentioned flexibility The test contact reverse side on surface (11) uniformly posts the resistance strain gage (9) in array distribution, above-mentioned flexible surface (11) bottom end It is also equipped with micro-inertial navigation module (8);Above-mentioned angular transducer (13), resistance strain gage (9) and micro-inertial navigation module (8) It is connect respectively by data/address bus with sensing data acquisition system (7);Sensing data acquisition system (7) and computer control terminal (6) it is communicated by data/address bus;
The test platform further includes X to sliding shoe (18), I fixed pulleys (19), II fixed pulleys (20), cord (22), counterweight Object (21) and wireless communication module (24);Wherein X is installed on roof supporting (16) to sliding shoe (18), and X is pushed up to sliding shoe (18) There is prismatic pair in X direction between end and roof supporting (16);I fixed pulleys (19) are identical with II fixed pulleys (20) holding Level height, they are fixed on X to sliding shoe (18) bottom end;Wireless communication module (24) is installed on legged type robot or adherency With animal;Computer control terminal(6)Be connected with host computer wireless communication module (5), host computer wireless communication module (5) with Robot wireless communication module (24) keeps wireless telecommunications;Cord (22) one end connection legged type robot main body (23) passes through the back of the body Band connection adheres to animal (28), and the other end coils through II fixed pulleys (20) and I fixed pulleys (19) successively, connects mass (21);
The test platform further includes X to high-speed camera (1), Y-direction high-speed camera (15), Z-direction high-speed camera (3);Wherein X To high-speed camera (1) along X-axis alignment flexible surface (11), Y-direction high-speed camera (15) is along Y-axis alignment flexible surface (11) Vertical side, Z-direction high-speed camera (3) are directed at flexible surface (11) horizontal side along Y-axis;X is high to high-speed camera (1), Y-direction Fast video camera (15) and Z-direction high-speed camera (3) are connected with computer control terminal (6) by data/address bus respectively.
2. special using the test method of the test platform of flexible surface adherency movement under simulated microgravity described in claim 1 Sign is to include following procedure:
Step 1, by legged type robot main body (23) or installation shoulder strap(27)Four-footed adherency animal (28) be suspended on cord (22) One end, cord (22) other end tie up to mass (21), and mass (21) and testee are equal in weight, and it is micro- heavy to constitute simulation Force environment condition;
Step 2 makes X be directed at testee to high-speed camera (1), Y-direction high-speed camera (15), Z-direction high-speed camera (3) And its observation area, believed in X, Y and Z-motion video image by computer control terminal (6) high-speed record testee Breath;
Step 3, computer control terminal (6) transmit a signal to robot wireless telecommunications by host computer wireless communication module (5) Module (24), the forms of motion of the four limbs and tail (25) of control legged type robot main body (23);
Uniformly distributed identical resistance strain gage (9) in step 4, flexible surface (11), forms m n array, flexible surface (11) it is curved The joint performance of quyi leads to resistance strain gage (9) resistance variations, and resistance strain gage (9) increased resistance value is acquired by sensing data acquisition system Flexible surface (11) bending curvature is measured indirectly, and bond material flexible surface (11) elasticity modulus measures flexible surface at this indirectly (11) moment of flexure and power, by determining resistance strain gage (9) in flexible surface (11) plane distribution position, you can acquire flexibility Moment of flexure everywhere in surface and force value;
Step 5 can cause flexible surface (11) to swing since adherency moves, in hinge(12)Locate setting angle sensor(13), Pass through sensing data acquisition system(7)Detect flexible surface(11)Angle of oscillation angle value;Flexible surface simultaneously(11)The micro- of bottom end is used to Property navigation module(8)The acceleration value and terminal angle angle in swing process are obtained, sensing data acquisition system is passed through(7)It adopts After collection, it is computer controlled terminal(6)It reads;
Step 6 is controlled by X to high-speed camera (1), Y-direction high-speed camera (15), Z-direction high-speed camera (3), computer Terminal(6)With sensing data acquisition system(7), have recorded legged type robot main body(23)Or four-footed adheres to animal(28)It is a variety of Move gait and flexible surface(11)Moment of flexure and power, oscillating acceleration and swing angle.
3. the test method that flexible surface adherency moves under simulated microgravity according to claim 2, it is characterised in that including Following procedure:
Utilize the flexible surface acquired in step 6(11)Moment of flexure and power, oscillating acceleration and swing angle and robot master Body(23)Or four-footed adheres to animal(28)Multi-motion gait video carries out the adherency exercise test under simulated microgravity.
4. the test method that flexible surface adherency moves under simulated microgravity according to claim 2, it is characterised in that including Following procedure:
Utilize the flexible surface acquired in step 6(11)Moment of flexure and power, oscillating acceleration and swing angle, as motion-sensing Feedback data, by computer control terminal(8)Corresponding movement gait data is taken, legged type robot main body is regulated and controled(23)'s Quadruped locomotion form and tail(25)Swing mode reaches holding flexible surface(11)The small control targe of chatter amplitude.
CN201810118313.5A 2018-02-06 2018-02-06 Test platform and measurement method for simulating adhesion motion of flexible surface under microgravity Active CN108394571B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810118313.5A CN108394571B (en) 2018-02-06 2018-02-06 Test platform and measurement method for simulating adhesion motion of flexible surface under microgravity

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810118313.5A CN108394571B (en) 2018-02-06 2018-02-06 Test platform and measurement method for simulating adhesion motion of flexible surface under microgravity

Publications (2)

Publication Number Publication Date
CN108394571A true CN108394571A (en) 2018-08-14
CN108394571B CN108394571B (en) 2021-02-12

Family

ID=63096313

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810118313.5A Active CN108394571B (en) 2018-02-06 2018-02-06 Test platform and measurement method for simulating adhesion motion of flexible surface under microgravity

Country Status (1)

Country Link
CN (1) CN108394571B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109752160A (en) * 2018-12-19 2019-05-14 上海航天控制技术研究所 Jet for space micro experimental rig resets rope and limits free destination apparatus
CN110393171A (en) * 2019-07-23 2019-11-01 南京航空航天大学 Insect spring behavior and mechanics observation system and test method
CN111806734A (en) * 2020-07-02 2020-10-23 中国人民解放军国防科技大学 Gravity compensation system, spacecraft relative motion ground suspension experiment system and method

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1947959A (en) * 2006-10-25 2007-04-18 哈尔滨工程大学 Wall gecko imitation mini-robot
CN101380235A (en) * 2008-09-24 2009-03-11 南京航空航天大学 Test method and system of animal foot-face contact counter force
CN103954555A (en) * 2014-03-17 2014-07-30 南京航空航天大学 Material adhesion/desorption performance testing system based on gecko bionic legs and self-regulation method
CN104697805A (en) * 2015-03-05 2015-06-10 南京航空航天大学 Test system and method for gecko aerial statue adjusting and landing motions
CN104859746A (en) * 2015-05-26 2015-08-26 南京航空航天大学 Experimental system and ground experimental method for gecko-inspired robot under micro-gravity environment
CN106515893A (en) * 2016-09-29 2017-03-22 南京航空航天大学 Force-sensing space-adaptive gecko inspired robot capable of fulfilling automatic adhesion and anti-adhesion functions and realizing attitude correction

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1947959A (en) * 2006-10-25 2007-04-18 哈尔滨工程大学 Wall gecko imitation mini-robot
CN101380235A (en) * 2008-09-24 2009-03-11 南京航空航天大学 Test method and system of animal foot-face contact counter force
CN103954555A (en) * 2014-03-17 2014-07-30 南京航空航天大学 Material adhesion/desorption performance testing system based on gecko bionic legs and self-regulation method
CN104697805A (en) * 2015-03-05 2015-06-10 南京航空航天大学 Test system and method for gecko aerial statue adjusting and landing motions
CN104859746A (en) * 2015-05-26 2015-08-26 南京航空航天大学 Experimental system and ground experimental method for gecko-inspired robot under micro-gravity environment
CN106515893A (en) * 2016-09-29 2017-03-22 南京航空航天大学 Force-sensing space-adaptive gecko inspired robot capable of fulfilling automatic adhesion and anti-adhesion functions and realizing attitude correction

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109752160A (en) * 2018-12-19 2019-05-14 上海航天控制技术研究所 Jet for space micro experimental rig resets rope and limits free destination apparatus
CN110393171A (en) * 2019-07-23 2019-11-01 南京航空航天大学 Insect spring behavior and mechanics observation system and test method
CN110393171B (en) * 2019-07-23 2021-07-27 南京航空航天大学 Insect bouncing behavior and mechanics observation method
CN111806734A (en) * 2020-07-02 2020-10-23 中国人民解放军国防科技大学 Gravity compensation system, spacecraft relative motion ground suspension experiment system and method
CN111806734B (en) * 2020-07-02 2022-06-07 中国人民解放军国防科技大学 Gravity compensation system, spacecraft relative motion ground suspension experiment system and method

Also Published As

Publication number Publication date
CN108394571B (en) 2021-02-12

Similar Documents

Publication Publication Date Title
CN108394571A (en) The test platform and measurement method of flexible surface adherency movement under simulated microgravity
CN106081173B (en) Three-dimensional active suspension type spacecraft microgravity simulator
CN106005497A (en) Suspension type six-degree-of-freedom micro-gravity environment simulating system
CN104697805B (en) Test system and method for gecko aerial statue adjusting and landing motions
CN102706361B (en) A kind of high precision many inertial navigation systems attitude accuracy assessment method
CN103869834B (en) Three-axis air-bearing table barycenter intelligent adjusting method based on empirical modal method
CN103091579A (en) Insulator chain intelligent detection robotic system
CN107867414B (en) Twelve-degree-of-freedom spacecraft simulator docking performance test device
CN107843775B (en) Three-dimensional electric field sonde capable of sensing thunderstorm cloud in gesture
CN109094817B (en) Carrier-based helicopter self-adaptive landing gear landing simulation system
CN103579736A (en) Mobile tracker for ship-borne antennas
CN207601192U (en) Posture can perceive thunder cloud three-dimensional electric field sonde
CN103868648A (en) Barycenter measuring method for three-axis air floatation simulation experiment platform
CN106005496A (en) Multi-point suspension active gravity compensation system
CN101510094B (en) Non-towing control double-torsion pendulum test device
CN109883642A (en) A kind of vehicle-mounted dynamometric system of low-speed operations device
CN108414175A (en) The vibration-testing and method of movement are adhered under simulated microgravity on elastic linear
CN100493654C (en) Discus used for testing athlete kinetics information
RU2561229C1 (en) Buoy for determination of characteristics of sea wind waves
CN113264203A (en) Multi-target six-degree-of-freedom microgravity ground simulation system and use method
CN114114918B (en) Stable control platform and stable control method for launching of marine rocket
CN113212816B (en) Suspension type four-degree-of-freedom motion simulation system and use method
CN203589188U (en) Level holding mechanism of onboard antenna tracking device
CN104678781B (en) Imitative gecko robot for space attitude regulation and control and landing experimental system and method
CN207758803U (en) A kind of track automatic measurement vehicle with sensor combinations

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant