CN109637290A - A kind of unmanned apparatus test device and its test macro - Google Patents
A kind of unmanned apparatus test device and its test macro Download PDFInfo
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- 238000012360 testing method Methods 0.000 title claims abstract description 162
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- 238000012545 processing Methods 0.000 claims description 38
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- 238000007664 blowing Methods 0.000 claims description 7
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- 238000001387 multinomial test Methods 0.000 description 1
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Abstract
A kind of unmanned apparatus test device and its test macro, including wind tunnel simulation test device, test flight device and real training exercise device；Wind tunnel simulation test device includes central blower, the first positioning shooting head, side blower, top bay, first base and bracket；Test flight device includes second base, the second positioning shooting head, lifting level ground, upper ramp, lower ramp, two groups of cylindrical bars, square piece and pennant；Real training exercise device includes third pedestal；Third pedestal is divided into virtual experience area, the first training center, the second training center and central control zone；The present invention is operated from the flight of all angles multiple no-manned plane and the respond of test operator, and tests comprehensively, good test effect.
Description
Technical field
The present invention relates to unmanned plane the field of test technology more particularly to a kind of unmanned apparatus test device and its test macros.
Background technique
Unmanned plane is using the not manned aircraft of radio robot and the presetting apparatus provided for oneself manipulation, extensively
Be applied to dual-use field.
Unmanned plane it is many kinds of, mainly include fixed-wing unmanned plane, flapping wing unmanned plane and multi-rotor unmanned aerial vehicle etc..Due to
Manipulation is simple, high reliablity, and do not need runway can VTOL, can hover in the sky after taking off, therefore opposite
In fixed-wing unmanned plane and flapping wing unmanned plane, multi-rotor unmanned aerial vehicle is widely applied in every field.More rotors nobody
Machine usually has 3 or more rotors, and mobility is realized by the torsion and revolving speed of the different rotors of change.Common is more
Rotor wing unmanned aerial vehicle is widely used in that video display are taken photo by plane, security monitoring, agricultural are planted such as quadrotor, six rotors and eight rotor wing unmanned aerial vehicles
It protects and the fields such as power-line patrolling.
Rotor wing unmanned aerial vehicle will be completed various tasks effectively, and the qualification and accuracy of operation are necessary, because
How unmanned operators are examined and be tested, be very important by this.
Summary of the invention
(1) goal of the invention
To solve technical problem present in background technique, the present invention proposes a kind of unmanned apparatus test device and its test system
System is operated and the respond of test operator from the flight of all angles multiple no-manned plane, and is tested comprehensively, test effect
Fruit is good.
(2) technical solution
To solve the above problems, the present invention provides a kind of unmanned apparatus test device, including wind tunnel simulation test device, fly
Row test device and real training exercise device；
Wind tunnel simulation test device includes central blower, the first positioning shooting head, side blower, top bay, the first bottom
Seat and bracket；
Bracket is vertically arranged, and pedestal upper end setting is arranged in first base in top bay bottom, the lower end of bracket；Side
On side blower rotation setting bracket, and spaced set is multiple along the vertical direction；Side blower blowing direction tilts upward and court
To test flight device center, to be centrally formed spiral air flow in test flight device；Central blower is arranged on top bay；
Air holes is set in first base, and air holes is correspondingly arranged with central blower along air-flow direction；The setting of first positioning shooting head exists
Top bay bottom, the first positioning shooting head are uniformly arranged multiple；First positioning shooting head and central processing system communication connection；
Test flight device includes second base, the second positioning shooting head, lifting level ground, upper ramp, lower ramp, two groups of cylinders
Bar, square piece and pennant；
Second positioning shooting head is arranged at the marginal position of second base, and the second positioning shooting head is transversely and longitudinal
Spaced set is multiple；Multiple second positioning shooting heads and central processing system communication connection；Go up and down level ground, upper ramp, lower ramp,
Two groups of cylindrical bars, square piece and pennant are arranged in second base；
Real training exercise device includes third pedestal；Third pedestal is divided into virtual experience area, the first training center, the second training
Area and central control zone；
Virtual experience area is equipped with VR virtual unit；First training center includes netted track and mobile robot；Mobile machine
People is slidably arranged on netted track, and mobile robot is equipped with for controlling the mobile tele-control system of mobile robot,
The tele-control system and central processing system control connect；Multiple lamps are uniformly arranged by square matrix arrangement in second training center
Column, lamppost top setting signal lamp；Central control room is set in central control zone；The centrally disposed control of central processing system
Room.
Preferably, the testing procedure of wind tunnel simulation test device 1 is as follows: AS1, and operator controls unmanned plane and flies into wind-tunnel mould
Inside quasi- test device, unmanned plane upper center is provided with the reflective spot captured for the first positioning shooting head；AS2 opens the
One positioning camera monitors unmanned plane in real time, and shooting picture is passed to central processing system；AS3, in opening
Entreat blower and multiple side blowers, random power, the power of side blower and the blowing for side blower for adjusting central blower
Wind angle and manufacture various simulated environments；Meanwhile operator controls unmanned plane and completes required movement in various simulated environments；
AS4 is analyzed by flight path of the central processing system to unmanned plane, and central processing system makes unmanned plane Performance Evaluation knot
Fruit, to determine acceptance or rejection.
Preferably, in wind tunnel simulation test: if colliding and damaging during unmanned plane during flying, judging unqualified；
If unmanned plane collisionless in flight course, determines qualification.
Preferably, the testing procedure of test flight device is as follows: BS1, multiple second positioning shooting heads is opened, to unmanned plane
It is monitored in real time, and shooting picture is passed into central processing system；Operator controls unmanned plane during flying in test flight
Above device；Wherein, the reflective spot captured for the second positioning shooting head is equipped with below unmanned plane；BS2, operator control nobody
Machine stops after falling on lifting level ground, then completes takeoff maneuver by lifting level ground；BS3, operator control unmanned plane respectively in upper ramp and
Climbing is completed on lower ramp to act with descending；BS4, operator control unmanned plane and fly around two groups of cylindrical bars in figure of eight track；
BS5, operator control unmanned plane and complete the flight of " mouth " font in square piece；BS6, operator control unmanned plane around pennant
Flight after a week, is flown to pennant；BS7, the BS2-BS6 the step of in, central processing system is to unmanned plane during flying
Track is analyzed, to determine acceptance or rejection.
Preferably, in test flight: in step BS3 and BS6, if unmanned plane during flying is no more than preset range, determining
It is qualified；In step BS4, drone flying height is no more than preset range, and flying height is no more than preset range, then determines
It is qualified；In step BS5, unmanned plane flies clockwise or counterclockwise, and flies within the scope of predetermined trajectory, then determines
It is qualified；Meanwhile any one is unqualified, determines that test flight is unqualified if determining in above step BS3-BS6.
Preferably, in real training exercise device, the use step of the first training center: CS1, user operate unmanned plane and fly the
Above one training center；CS2, central processing system control mobile robot random movement on netted track；CS3, operator's control
The head of unmanned plane processed is always towards mobile robot.
Preferably, in real training exercise device, the use step of the second training center: DS1, user operate unmanned plane and fly the
Above two training centers；DS2, central processing system random controling signal lamp are lighted one by one；DS3, operator control unmanned plane and fly again
The top for the signal lamp being lit.
In the present invention, according to above-mentioned unmanned apparatus test device, it is also proposed that a kind of test macro of unmanned apparatus test device,
It is characterized in that, comprising the following steps:
S1, operator control unmanned plane and complete wind tunnel simulation test by wind tunnel simulation test device 1；
S2, operator control unmanned plane and complete test flight by test flight device 2；
In step S1 and S2, central processing system determines that wind tunnel simulation test and test flight are qualified, then determines nothing
Man-machine test passes；Conversely, determining unqualified.
Above-mentioned technical proposal of the invention has following beneficial technical effect: wind tunnel simulation test device passes through in adjusting
Centre blower and side blower blow the size of wind speed inside regulating device, simultaneously, additionally it is possible to by the blowing angle for adjusting side blower
Degree adjusts the variation of wind direction, and realizes the environment such as spiral air flow；Equipment is by simulating different working environments to unmanned plane
And the operation of unmanned plane is tested, good test effect；Wherein, air holes is set in first base, and air holes, which has, realizes gas
The effect of circulation, air holes also have the function of being afraid of that sundries out is discharged unmanned plane remains, avoids damaging especially when unmanned plane damages
Bad center blower and side blower.Test flight device include lifting level ground, upper ramp, lower ramp, two groups of cylindrical bars, square piece and
The multiple test components of pennant, be respectively used to the test lifting of unmanned plane, climbing, descending, the flight of " " word, the flight of " mouth " word and around
Flag flight tests the flexibility and stability of unmanned plane to test the various flying methods without popularity and take a lot of trouble track；Real training is practiced
It practises dress and centers virtual experience area, people can be allowed to rest, moreover it is possible to operator be allowed to experience using VR virtual unit；Its
In, the first training center and the second training center are capable of the respond and flexible ability of test operator, and test nobody simultaneously
The flying distance of machine controls, good test effect.Wherein, the first positioning shooting head and the second positioning shooting head can complete monitoring without
Shooting picture is passed to central processing system by man-machine flight course, biscuit, observation and record convenient for examination personnel, and first
Positioning shooting head and the second positioning shooting head are respectively provided with multiple, realize comprehensive no dead angle shooting, guarantee the accuracy of test.
To sum up, the present invention operates and the respond of test operator from the flight of all angles multiple no-manned plane, and
Test is comprehensive, good test effect.
Detailed description of the invention
Fig. 1 is that the structure of wind-tunnel simulating test device in unmanned apparatus test device proposed by the present invention and its test macro is shown
It is intended to.
Fig. 2 is the structural representation of test flight device in unmanned apparatus test device proposed by the present invention and its test macro
Figure.
Fig. 3 is the structural representation of real training exercise device in unmanned apparatus test device proposed by the present invention and its test macro
Figure.
Fig. 4 is system flow schematic diagram in unmanned apparatus test device proposed by the present invention and its test macro.
Specific embodiment
In order to make the objectives, technical solutions and advantages of the present invention clearer, With reference to embodiment and join
According to attached drawing, the present invention is described in more detail.It should be understood that these descriptions are merely illustrative, and it is not intended to limit this hair
Bright range.In addition, in the following description, descriptions of well-known structures and technologies are omitted, to avoid this is unnecessarily obscured
The concept of invention.
Fig. 1 is that the structure of wind-tunnel simulating test device in unmanned apparatus test device proposed by the present invention and its test macro is shown
It is intended to.
Fig. 2 is the structural representation of test flight device in unmanned apparatus test device proposed by the present invention and its test macro
Figure.
Fig. 3 is the structural representation of real training exercise device in unmanned apparatus test device proposed by the present invention and its test macro
Figure.
As shown in Figure 1-3, a kind of unmanned apparatus test device proposed by the present invention and its test macro, including wind tunnel simulation are surveyed
1, test flight device 2 and real training exercise device 3 are set in trial assembly；
Wind tunnel simulation test device 1 includes central blower 11, the first positioning shooting head 12, side blower 13, top bay
15, first base 16 and bracket 17；
Bracket 17 is vertically arranged, and the setting of 17 upper end of bracket is arranged in 15 bottom of top bay, the lower end of bracket 17 first
On pedestal 16；On the rotation setting bracket 17 of side blower 13, and spaced set is multiple along the vertical direction；Side blower 13 is dried
Direction tilts upward and towards test flight device center, to be centrally formed spiral air flow in test flight device；Central blower
11 are arranged on top bay 15；Air holes 14 is set in first base 16, and air holes 14 and central blower 11 are along air-flow direction
It is correspondingly arranged；First positioning shooting head 12 is arranged in 15 bottom of top bay, and the first positioning shooting head 12 is uniformly arranged multiple；The
One positioning camera 12 and central processing system communication connection；
Test flight device includes second base 20, the second positioning shooting head 21, lifting level ground 22, upper ramp 23, lower ramp
24, two groups of cylindrical bars 25, square piece 26 and pennant 27；
Second positioning shooting head 21 is arranged at the marginal position of second base 20, and the second positioning shooting head 21 is transversely
And longitudinal direction spaced set is multiple；Multiple second positioning shooting heads 21 and central processing system communication connection；It goes up and down level ground 22, go up a slope
Platform 23,24, two groups of cylindrical bars 25 of lower ramp, square piece 26 and pennant 27 are arranged in second base 20；
Real training exercise device 3 includes third pedestal 30；Third pedestal 30 is divided into virtual experience area 31, the first training center
32, the second training center 33 and central control zone 34；
Virtual experience area 31 is equipped with VR virtual unit；First training center 32 includes netted track 35 and mobile robot 35；
Mobile robot 35 is slidably arranged on netted track 35, and mobile robot 35 is equipped with mobile for controlling mobile robot 35
Tele-control system, the tele-control system and central processing system control connect；Square matrix is pressed in second training center 33
Arrangement is uniformly arranged multiple lampposts 37,37 top setting signal lamp of lamppost；Central control room is set in central control zone 34；Center
The centrally disposed control room of processing system.
In the present invention, wind tunnel simulation test device 1 is blown in regulating device by adjusting central blower 11 and side blower 13
The size of portion's wind speed, simultaneously, additionally it is possible to which the blowing angle by adjusting side blower 13 adjusts the variation of wind direction, and realizes spiral shell
The environment such as rotational gas flow；Equipment tests the operation of unmanned plane and unmanned plane by simulating different working environments, surveys
It is good to try effect；Wherein, air holes 14 is set in first base 16, and air holes has the function of realizing gas circulation, and air holes 14 also has
Be afraid of that the function of sundries out is discharged unmanned plane remains, avoids damaging central blower 11 and side blower especially when unmanned plane damages
13.Test flight device 2 includes lifting level ground 22, upper ramp 23,24, two groups of cylindrical bars 25 of lower ramp, square piece 26 and pennant
A test component more than 27 is respectively used to the test lifting of unmanned plane, climbing, descending, the flight of " 8 " word, " mouth " word flight and around flag
Flight tests the flexibility and stability of unmanned plane to test the various flying methods without popularity and take a lot of trouble track；Real training practice
Virtual experience area 31 is set in device 3, people can be allowed to rest, moreover it is possible to operator be allowed to experience using VR virtual unit；Its
In, the first training center 32 and the second training center 33 are capable of the respond and flexible ability of test operator, and test simultaneously
The flying distance of unmanned plane controls, good test effect.
In the present invention, the first positioning shooting head 12 and the second positioning shooting head 21 are capable of the flight of complete monitoring unmanned plane
Shooting picture is passed to central processing system by journey, biscuit, convenient for examining observation and the record of personnel, the first positioning shooting head 12
It is respectively provided with the second positioning shooting head 21 multiple, realizes comprehensive no dead angle shooting, guarantee the accuracy of test.
To sum up, the present invention operates and the respond of test operator from the flight of all angles multiple no-manned plane, and
Test is comprehensive, good test effect.
In an alternative embodiment, the testing procedure of wind tunnel simulation test device 1 is as follows:
AS1, operator control unmanned plane and fly into inside wind tunnel simulation test device 1, and the setting of unmanned plane upper center is useful
In the reflective spot that the first positioning shooting head 12 captures；
AS2 opens the first positioning shooting head 12 and monitors in real time to unmanned plane, and shooting picture is passed to center
Processing system；
AS3 opens central blower 11 and multiple side blowers 13, random power, the side wind for adjusting central blower 11
The power of machine 13 and the blowing angle of side blower 13 and manufacture various simulated environments；Meanwhile operator controls unmanned plane and exists
Required movement is completed in various simulated environments；
AS4 is analyzed by flight path of the central processing system to unmanned plane, and central processing system makes unmanned plane
Energy assessment result, to determine acceptance or rejection.
In an alternative embodiment, in wind tunnel simulation test: if colliding and damaging during unmanned plane during flying,
It then judges unqualified；If unmanned plane collisionless in flight course, determines qualification.
It should be noted that in testing, flying and adjusting according to different solemn Buddhist nun's environment, to check nobody
The flying quality of machine and the respond of operator, test effect are fine.Wherein, reflective spot is arranged in unmanned plane upper center,
In order to the quick and effective capture of the first positioning shooting head 12, guarantee reaches best condition to the shooting of unmanned plane, in order to
The judgement of central processing system.
In an alternative embodiment, the testing procedure of test flight device 2 is as follows:
BS1 opens multiple second positioning shooting heads 21, monitors in real time to unmanned plane, and shooting picture is transmitted
To central processing system；Operator controls unmanned plane during flying above test flight device 2；Wherein, it is equipped with and uses below unmanned plane
In the reflective spot that the second positioning shooting head 21 captures；
BS2, operator controls unmanned plane and stops after falling on lifting level ground 22, then completes takeoff maneuver by lifting level ground 22；
BS3, operator control unmanned plane and complete climbing and descending movement on upper ramp 23 and lower ramp 24 respectively；
BS4, operator control unmanned plane and fly around two groups of cylindrical bars 25 in figure of eight track；
BS5, operator control unmanned plane and complete the flight of " mouth " font in square piece 26；
BS6, operator controls unmanned plane and flies after a week around pennant 27, right above flight to pennant 27；
BS7, the BS2-BS6 the step of in, central processing system analyzes unmanned plane during flying track, to determine qualification
Or it is unqualified.
In an alternative embodiment, in test flight: in step BS3 and BS6, if unmanned plane during flying is no more than in advance
If range then determines qualification；In step BS4, drone flying height is no more than preset range, and flying height is no more than in advance
If range then determines qualification；In step BS5, unmanned plane flies clockwise or counterclockwise, and flies in predetermined trajectory
In range, then qualification is determined；Meanwhile any one is unqualified, determines test flight not if determining in above step BS3-BS6
It is qualified.
It should be noted that test flight device 2 carries out multinomial test to unmanned plane, fly to test the various of unmanned plane
Row motion mode and flight path, to test the comprehensive performance of unmanned plane, good test effect comprehensively.Wherein, before testing, it needs
Preset range is made to the flight path of unmanned plane, using as judge unmanned plane during flying whether He Ge condition.
In an alternative embodiment, in real training exercise device 3, the use step of the first training center 32:
CS1, user operate unmanned plane and fly above the first training center 32；
CS2, central processing system control the random movement on netted track 35 of mobile robot 35；
CS3, operator control the head of unmanned plane always towards mobile robot 35.
In an alternative embodiment, in real training exercise device 3, the use step of the second training center 33:
DS1, user operate unmanned plane and fly above the second training center 33；
DS2, central processing system random controling signal lamp are lighted one by one；
DS3, operator control the top that unmanned plane flies the signal lamp being lit again.
It should be noted that the first training center 32 and 33 military affairs of the second training center are used to test the anti-of unmanned operators
Should be able to power, and to the judgement of unmanned plane during flying track, practice is convenient, and practice effect is good.Wherein, it before practice, needs
Regulation is made to the flying method of unmanned plane, to improve the effect of practice unmanned plane during flying, is surveyed consequently facilitating completing wind tunnel simulation
Examination and test flight.
Fig. 4 is system flow schematic diagram in unmanned apparatus test device proposed by the present invention and its test macro.
The present invention is according to above-mentioned unmanned apparatus test device, it is also proposed that a kind of test macro of unmanned apparatus test device, it is special
Sign is, comprising the following steps:
S1, operator control unmanned plane and complete wind tunnel simulation test by wind tunnel simulation test device 1；
S2, operator control unmanned plane and complete test flight by test flight device 2；
In step S1 and S2, central processing system determines that wind tunnel simulation test and test flight are qualified, then determines nothing
Man-machine test passes；Conversely, determining unqualified
It should be noted that containing multiple test items in test flight, it is necessary to which all items determine qualification, then could
Enough determine that test flight is qualified.In the present invention, the comprehensive test to unmanned plane is realized, and do to the respond of operator
It tests out, apparatus is simple, good test effect, and test method is convenient for implementation.
It should be understood that above-mentioned specific embodiment of the invention is used only for exemplary illustration or explains of the invention
Principle, but not to limit the present invention.Therefore, that is done without departing from the spirit and scope of the present invention is any
Modification, equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.In addition, appended claims purport of the present invention
Covering the whole variations fallen into attached claim scope and boundary or this range and the equivalent form on boundary and is repairing
Change example.
Claims (8)
1. a kind of unmanned apparatus test device, which is characterized in that including wind tunnel simulation test device (1), test flight device (2) and
Real training exercise device (3)；
Wind tunnel simulation test device (1) includes central blower (11), the first positioning shooting head (12), side blower (13), top
Rack (15), first base (16) and bracket (17)；
Bracket (17) is vertically arranged, and the setting of bracket (17) upper end exists in top bay (15) bottom, the lower end setting of bracket (17)
In first base (16)；In side blower (13) rotation setting bracket (17), and spaced set is multiple along the vertical direction；Side
Blower (13) blowing direction tilts upward and towards test flight device center, to be centrally formed spiral gas in test flight device
Stream；Central blower (11) is arranged on top bay (15)；Air holes (14) are set in first base (16), air holes (14) and center
Blower (11) is correspondingly arranged along air-flow direction；The setting of first positioning shooting head (12) is in top bay (15) bottom, and first
Positioning shooting head (12) is uniformly arranged multiple；First positioning shooting head (12) and central processing system communication connection；
Test flight device include second base (20), the second positioning shooting head (21), lifting level ground (22), upper ramp (23), under
Ramp (24), two groups of cylindrical bars (25), square piece (26) and pennant (27)；
Second positioning shooting head (21) is arranged at the marginal position of second base (20), and the second positioning shooting head (21) is along cross
To and longitudinal spaced set it is multiple；Multiple second positioning shooting heads (21) and central processing system communication connection；Go up and down level ground
(22), upper ramp (23), lower ramp (24), two groups of cylindrical bars (25), square piece (26) and pennant (27) are arranged at second
On pedestal (20)；
Real training exercise device (3) includes third pedestal (30)；Third pedestal (30) is divided into virtual experience area (31), the first training
Area (32), the second training center (33) and central control zone (34)；
Virtual experience area (31) is equipped with VR virtual unit；First training center (32) includes netted track (35) and mobile robot
(35)；Mobile robot (35) is slidably arranged on netted track (35), and mobile robot (35) is equipped with for controlling movement
The mobile tele-control system of robot (35), the tele-control system and central processing system control connect；Second training center
(33) it is uniformly arranged multiple lampposts (37) in by square matrix arrangement, setting signal lamp at the top of lamppost (37)；Central control zone
(34) central control room is set in；The centrally disposed control room of central processing system.
2. unmanned apparatus test device according to claim 1, which is characterized in that the test of wind tunnel simulation test device (1)
Steps are as follows:
AS1, operator control unmanned plane and fly into wind tunnel simulation test device (1) inside, and unmanned plane upper center, which is provided with, to be used for
The reflective spot that first positioning shooting head (12) captures；
AS2 opens the first positioning shooting head (12) and monitors in real time to unmanned plane, and shooting picture is passed to centre
Reason system；
AS3 opens central blower (11) and multiple side blowers (13), the random power for adjusting central blower (11), side
The power of blower (13) and the blowing angle of side blower (13) and manufacture various simulated environments；Meanwhile operator controls nothing
It is man-machine to complete required movement in various simulated environments；
AS4 is analyzed by flight path of the central processing system to unmanned plane, and central processing system is made unmanned plane performance and commented
Estimate as a result, to determine acceptance or rejection.
3. unmanned apparatus test device according to claim 2, which is characterized in that in wind tunnel simulation test: if unmanned plane flies
It collides and damages during row, then judge unqualified；If unmanned plane collisionless in flight course, determines qualification.
4. unmanned apparatus test device according to claim 1, which is characterized in that the testing procedure of test flight device (2)
It is as follows:
BS1 opens multiple second positioning shooting heads (21), monitors in real time to unmanned plane, and shooting picture is passed to
Central processing system；Operator controls unmanned plane during flying above test flight device (2)；Wherein, it is equipped with and uses below unmanned plane
In the reflective spot that the second positioning shooting head (21) captures；
BS2, operator controls unmanned plane and stops after falling in lifting level ground (22), then completes takeoff maneuver by lifting level ground (22)；
BS3, operator control unmanned plane and complete climbing and descending movement on upper ramp (23) and lower ramp (24) respectively；
BS4, operator control unmanned plane and fly around two groups of cylindrical bars (25) in figure of eight track；
BS5, operator control unmanned plane and complete the flight of " mouth " font in square piece (26)；
BS6, operator controls unmanned plane and flies after a week around pennant (27), right above flight to pennant (27)；
BS7, the BS2-BS6 the step of in, central processing system analyzes unmanned plane during flying track, qualified or not to determine
It is qualified.
5. unmanned apparatus test device according to claim 4, which is characterized in that in test flight: in step BS3 and BS6
In, if unmanned plane during flying is no more than preset range, determine qualification；In step BS4, drone flying height is no more than default
Range, and flying height is no more than preset range, then determines qualification；In step BS5, unmanned plane is along side clockwise or counterclockwise
It to flight, and flies within the scope of predetermined trajectory, then determines qualification；Meanwhile if any one is determined in above step BS3-BS6
It is unqualified, then determine that test flight is unqualified.
6. unmanned apparatus test device according to claim 1, which is characterized in that in real training exercise device (3), the first training
The use step in area (32):
CS1, user operate unmanned plane and fly above the first training center (32)；
CS2, central processing system control mobile robot (35) random movement on netted track (35)；
CS3, operator control the head of unmanned plane always towards mobile robot (35).
7. unmanned apparatus test device according to claim 1, which is characterized in that in real training exercise device (3), the second training
The use step in area (33):
DS1, user operate unmanned plane and fly above the second training center (33)；
DS2, central processing system random controling signal lamp are lighted one by one；
DS3, operator control the top that unmanned plane flies the signal lamp being lit again.
8. unmanned apparatus test device according to claim 1-7, it is also proposed that a kind of survey of unmanned apparatus test device
Test system, which comprises the following steps:
S1, operator control unmanned plane and complete wind tunnel simulation test by wind tunnel simulation test device (1)；
S2, operator control unmanned plane and complete test flight by test flight device (2)；
In step S1 and S2, central processing system determines that wind tunnel simulation test and test flight are qualified, then determines unmanned plane
Test passes；Conversely, determining unqualified.
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