CN110654560A - Vehicle-mounted unmanned aerial vehicle control system and control method thereof - Google Patents
Vehicle-mounted unmanned aerial vehicle control system and control method thereof Download PDFInfo
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- CN110654560A CN110654560A CN201910813589.XA CN201910813589A CN110654560A CN 110654560 A CN110654560 A CN 110654560A CN 201910813589 A CN201910813589 A CN 201910813589A CN 110654560 A CN110654560 A CN 110654560A
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- 238000000034 method Methods 0.000 title claims abstract description 8
- 238000001514 detection method Methods 0.000 claims abstract description 25
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 28
- 239000000741 silica gel Substances 0.000 claims description 28
- 229910002027 silica gel Inorganic materials 0.000 claims description 28
- 230000003139 buffering effect Effects 0.000 claims description 19
- 239000004744 fabric Substances 0.000 claims description 19
- 239000000919 ceramic Substances 0.000 claims description 10
- 241000252254 Catostomidae Species 0.000 claims description 5
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 238000002360 preparation method Methods 0.000 claims description 3
- 108010066057 cabin-1 Proteins 0.000 description 24
- 101100190621 Arabidopsis thaliana PLC4 gene Proteins 0.000 description 10
- 230000004888 barrier function Effects 0.000 description 9
- 230000005540 biological transmission Effects 0.000 description 8
- 238000005452 bending Methods 0.000 description 4
- 239000006185 dispersion Substances 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Launching or towing gear
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/16—Aircraft characterised by the type or position of power plant of jet type
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/15—Propulsion using combustion exhausts other than turbojets or turbofans, e.g. using rockets, ramjets, scramjets or pulse-reactors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
Abstract
The invention discloses a vehicle-mounted unmanned aerial vehicle control system and a control method thereof, and the vehicle-mounted unmanned aerial vehicle control system comprises a square tube launching cabin, an extension section, an electric rotary table, a PLC (programmable logic controller) and a terminal, wherein the head end of the square tube launching cabin is hinged with the electric rotary table, an unmanned aerial vehicle position detection device is arranged in the square tube launching cabin, an obstacle sensor is arranged at the tail end of the square tube launching cabin, a first electric guide rail is embedded on the inner bottom surface of the square tube launching cabin, a second electric guide rail is embedded on the outer bottom surface of the square tube launching cabin, a following plate is arranged on the first electric guide rail, the left side wall and the right side wall of the square tube launching cabin are both provided with guide ports matched with wings of an unmanned aerial vehicle, ball rows are arranged on the guide ports, a dovetail groove is formed in the outer bottom surface of the square tube; the vehicle-mounted unmanned aerial vehicle control system is high in automation degree.
Description
This patent is the divisional application, and the original case application information is: 10/13/2017, application number 2017109509951 entitled: a vehicle-mounted unmanned aerial vehicle control system and a control method thereof.
Technical Field
The invention relates to a vehicle-mounted unmanned aerial vehicle control system and a control method thereof.
Background
The pulse jet engine is one of jet engines and can be used on a target aircraft, a missile or an aviation model. German Nykul was used to propel V-1 missiles, bombing London, in the late world war II. The pulse jet engine has simple structure, convenient processing and higher combustion efficiency than the common internal combustion engine, thus being applicable to various aviation and sea models.
At present, the pulse jet type unmanned aerial vehicle is not suitable for taking off in a vehicle-mounted environment, and a technical person in the field hopes that an auxiliary system which can take off in the vehicle-mounted environment by the pulse jet type unmanned aerial vehicle can be developed, so that the flexibility of the pulse jet type is improved.
Disclosure of Invention
The invention provides a vehicle-mounted unmanned aerial vehicle control system for solving the technical problems, the system has high automation degree, and the pulsed jet unmanned aerial vehicle using the system can take off in a vehicle-mounted environment.
In order to solve the problems, the invention adopts the following technical scheme:
a vehicle-mounted unmanned aerial vehicle control system comprises a square tube launching cabin, an extension section, an electric rotary table, a PLC (programmable logic controller) and a terminal, wherein the head end of the square tube launching cabin is hinged with the electric rotary table, an unmanned aerial vehicle position detection device is arranged in the square tube launching cabin, an obstacle sensor is arranged at the tail end of the square tube launching cabin, a first electric guide rail is inlaid on the inner bottom surface of the square tube launching cabin, a second electric guide rail is inlaid on the outer bottom surface of the square tube launching cabin, a following plate is arranged on the first electric guide rail, the left side wall and the right side wall of the square tube launching cabin are respectively provided with a guide port matched with wings of the unmanned aerial vehicle, a ball row is arranged on each guide port, a dovetail groove is formed in the outer bottom surface of the square tube launching cabin, a dovetail matched with the dovetail groove is arranged on the extension section, the dovetail is inserted into the dovetail groove, the extension section is linked with the second electric guide rail, the electric rotary table, the unmanned aerial vehicle position detection device, the first electric guide rail and the second electric guide rail are electrically connected with the PLC, and the terminal is connected with the PLC in a data mode.
Preferably, an electric telescopic rod is arranged between the electric rotary table and the square pipe launching cabin, two ends of the electric telescopic rod are respectively hinged with the electric rotary table and the square pipe launching cabin, the electric telescopic rod is electrically connected with the PLC, and the PLC can drive the electric telescopic rod to adjust the inclination of the square pipe launching cabin.
As preferred, unmanned aerial vehicle position detecting device includes infrared emission pipe and infrared ray receiver tube, infrared emission pipe and infrared ray receiver tube are in the face of setting up, infrared emission pipe and infrared ray receiver tube are installed respectively in two diagonal departments in square pipe transmission cabin, infrared emission pipe and infrared ray receiver tube all are provided with more than one, infrared emission pipe and infrared ray receiver tube are equidistant distribution, adopt infrared emission pipe and infrared ray receiver tube to survey, and the accuracy is high to two diagonal departments of installing in square pipe transmission cabin can avoid being strikeed.
As preferred, the follow board back is provided with the silica gel connecting strip, the silica gel connecting strip is the right angle form setting, silica gel connecting strip one side and follow board bolted connection, the slider bolted connection of silica gel connecting strip another side and first electronic guide rail, the slider of follow board and first electronic guide rail passes through the silica gel connecting strip and connects, and when the follow board struck unmanned aerial vehicle, the silica gel connecting strip can absorb and the impact of dispersion through the bending, prevents that unmanned aerial vehicle from being damaged by the collision.
As preferred, the follow board is the cavity setting, follow the board front side and be provided with thermal-insulated ceramic plate, follow board and thermal-insulated ceramic plate mortise-tenon joint, follow the board and adopted hollow design, the burden that can the first electronic guide rail of effectual reduction, light in weight moreover.
Preferably, the bottom surface of the electric turntable is provided with the vacuum chucks, the vacuum chucks are in threaded connection with the electric turntable and are arranged in more than one mode, the vacuum chucks are distributed in an annular array mode, and the vacuum chucks are arranged on the bottom surface of the electric turntable, so that a user can be conveniently connected with an automobile.
Preferably, be provided with buffering elasticity cloth on the guiding opening, buffering elasticity cloth both ends all with square pipe launch cabin riveting, buffering elasticity cloth is mutually perpendicular with the ball row, through be provided with buffering elasticity cloth on the guiding opening, unmanned aerial vehicle's wing direct impact to square pipe launch cabin when can preventing to put into unmanned aerial vehicle.
Preferably, the extension section is connected with the slider bolt of the second electric guide rail, and the extension section is conveniently detached from the slider of the second electric guide rail and reliably connected with the slider of the second electric guide rail.
Another technical problem to be solved by the present invention is to provide a control method for a vehicle-mounted unmanned aerial vehicle control system, which is characterized by comprising the following steps:
1) the PLC starts the unmanned aerial vehicle position detection device and the obstacle sensor for detection immediately after receiving a takeoff preparation signal sent by the terminal;
2) when the obstacle sensor detects that an obstacle exists in 20-40 meters, a signal is fed back to the PLC, and the PLC controls the electric rotary table to adjust the direction of the square tube launching cabin until no obstacle exists in 20-40 meters;
3) the PLC drives the second electric guide rail to unfold the extension section and then feeds a takeoff enabling signal back to the terminal;
4) starting the pulse jet unmanned aerial vehicle;
5) once the detection device detects that the pulse jet unmanned aerial vehicle moves in the square tube launching cabin, the signal is fed back to the PLC, the PLC drives the first electric guide rail to enable the following plate to follow the pulse jet unmanned aerial vehicle, and the pulse jet unmanned aerial vehicle can obtain good reaction force when taking off in the square tube launching cabin;
5) after the first electric guide rail reaches the maximum stroke, a signal is fed back to the PLC, and the PLC controls the first electric guide rail and the first electric guide rail to reset and stops the unmanned aerial vehicle position detection device and the obstacle sensor to work.
The invention has the beneficial effects that: through being provided with the condition that electric turntable and obstacle sensor cooperation PLC can effectual detection external obstacle under the on-vehicle condition, the departure angle of real-time adjustment unmanned aerial vehicle prevents that unmanned aerial vehicle from striking the obstacle after the departure, very be fit for using under on-vehicle condition, can satisfy the vehicle and take off under the condition of traveling, and degree of automation is high, in addition, be provided with electric telescopic handle between electric turntable and the square pipe launch cabin, the electric telescopic handle both ends are connected with electric turntable and square pipe launch cabin are articulated respectively, electric telescopic handle and PLC electric connection, PLC can drive electric telescopic handle and adjust the gradient in square pipe launch cabin. Unmanned aerial vehicle position detecting device includes infrared emission pipe and infrared ray receiver tube, infrared emission pipe and infrared ray receiver tube are in the face of setting, infrared emission pipe and infrared ray receiver tube are installed respectively in two diagonal departments in square pipe transmission cabin, infrared emission pipe and infrared ray receiver tube all are provided with more than one, infrared emission pipe and infrared ray receiver tube are equidistant distribution, adopt infrared emission pipe and infrared ray receiver tube to survey, the accuracy is high, and install two diagonal departments in square pipe transmission cabin and can avoid being strikeed. Follow the board back and be provided with the silica gel connecting strip, the silica gel connecting strip is the right angle form setting, silica gel connecting strip one side and follow board bolted connection, silica gel connecting strip another side and the slider bolted connection of first electronic guide rail, follow the board and pass through the silica gel connecting strip with the slider of first electronic guide rail and be connected, when the follow board strikes unmanned aerial vehicle, the silica gel connecting strip can absorb the impact with the dispersion through the bending, prevent that unmanned aerial vehicle from being damaged. Follow the board and be the cavity setting, follow the board and be provided with thermal-insulated ceramic plate on the front, follow board and thermal-insulated ceramic plate mortise-tenon joint, follow the board and adopted hollow design, the burden that can the first electronic guide rail of effectual reduction, weight is light moreover. The bottom surface of the electric turntable is provided with more than one vacuum sucker, the vacuum suckers are in threaded connection with the electric turntable and distributed in an annular array, and the vacuum suckers are arranged on the bottom surface of the electric turntable, so that a user can conveniently connect with an automobile. Be provided with buffering elasticity cloth on the guide way, buffering elasticity cloth both ends all with square pipe launch cabin riveting, buffering elasticity cloth is arranged mutually perpendicularly with the ball, through be provided with buffering elasticity cloth on the guide way, unmanned aerial vehicle's wing directly strikes square pipe launch cabin when can preventing to put into unmanned aerial vehicle. The extension section is connected with the slider bolt of the second electric guide rail, and the extension section is convenient to disassemble and assemble with the slider of the second electric guide rail and is reliable in connection.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
Fig. 1 is a perspective view of a vehicle-mounted unmanned aerial vehicle control system of the present invention;
FIG. 2 is a cross-sectional view of a square tube launch cabin of a vehicle-mounted unmanned aerial vehicle control system of the present invention;
fig. 3 is a perspective view of a follower plate of a vehicle-mounted unmanned aerial vehicle control system of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
Example 1
As shown in fig. 1-3, a vehicle-mounted unmanned aerial vehicle control system comprises a square tube launching cabin 1, an extension section 2, an electric rotary table 3, a PLC4 and a terminal (not shown), wherein the head end of the square tube launching cabin 1 is hinged with the electric rotary table 3, an unmanned aerial vehicle position detecting device is arranged in the square tube launching cabin 1, an obstacle sensor 5 is arranged at the tail end of the square tube launching cabin 1, a first electric guide rail 6 is embedded on the inner bottom surface of the square tube launching cabin 1, a second electric guide rail (not shown) is embedded on the outer bottom surface of the square tube launching cabin 1, a following plate 7 is arranged on the first electric guide rail 6, guide ports 8 matched with wings of the unmanned aerial vehicle are arranged on the left side wall and the right side wall of the square tube launching cabin 1, a ball row 9 is arranged on the guide port 8, a dovetail groove (not shown) is formed on the outer bottom surface of the square tube launching cabin 1, a dovetail 10, dovetail 10 inserts in the dovetail, square pipe launch cabin 1 passes through dovetail and dovetail 10 sliding connection with extension section 2, extension section 2 and the electronic guide rail interlock of second, electronic revolving stage 3, unmanned aerial vehicle position detection device, first electronic guide rail 6 and the electronic guide rail of second all with PLC4 electric connection, the terminal passes through the data line with PLC4 and is connected. Through being provided with the condition that electronic revolving stage 3 and barrier sensor 5 cooperation PLC4 can effectual detection external barrier under the on-vehicle condition, the departure angle of real-time adjustment unmanned aerial vehicle prevents that unmanned aerial vehicle from striking the barrier after the departure, and very suitable use under the on-vehicle condition can satisfy the vehicle and take off under the condition of traveling, and degree of automation is high moreover.
The beneficial effect of this embodiment does: through being provided with the circumstances that electronic revolving stage and barrier sensor cooperation PLC can effectual detection external barrier under the on-vehicle circumstances, real-time adjustment unmanned aerial vehicle's departure angle prevents that unmanned aerial vehicle from striking the barrier after the departure, and very suitable use under the on-vehicle circumstances can satisfy the vehicle and take off under the circumstances of traveling, and degree of automation is high moreover.
Example 2
As shown in fig. 1-3, a vehicle-mounted unmanned aerial vehicle control system comprises a square tube launching cabin 1, an extension section 2, an electric rotary table 3, a PLC4 and a terminal (not shown), wherein the head end of the square tube launching cabin 1 is hinged with the electric rotary table 3, an unmanned aerial vehicle position detecting device is arranged in the square tube launching cabin 1, an obstacle sensor 5 is arranged at the tail end of the square tube launching cabin 1, a first electric guide rail 6 is embedded on the inner bottom surface of the square tube launching cabin 1, a second electric guide rail (not shown) is embedded on the outer bottom surface of the square tube launching cabin 1, a following plate 7 is arranged on the first electric guide rail 6, guide ports 8 matched with wings of the unmanned aerial vehicle are arranged on the left side wall and the right side wall of the square tube launching cabin 1, a ball row 9 is arranged on the guide port 8, a dovetail groove (not shown) is formed on the outer bottom surface of the square tube launching cabin 1, a dovetail 10, dovetail 10 inserts in the dovetail, square pipe launch cabin 1 passes through dovetail and dovetail 10 sliding connection with extension section 2, extension section 2 and the electronic guide rail interlock of second, electronic revolving stage 3, unmanned aerial vehicle position detection device, first electronic guide rail 6 and the electronic guide rail of second all with PLC4 electric connection, the terminal passes through the data line with PLC4 and is connected. Be provided with electric telescopic handle 11 between electric turntable 3 and the square pipe launch cabin 1, electric telescopic handle 11 both ends are connected with electric turntable 3 and square pipe launch cabin 1 is articulated respectively, electric telescopic handle 11 and PLC4 electric connection, PLC4 can drive electric telescopic handle 11 and adjust the gradient in square pipe launch cabin 1. Unmanned aerial vehicle position detection device includes infrared emission pipe 12 and infrared ray receiver tube 13, infrared emission pipe 12 and infrared ray receiver tube 13 are in the face of setting up, infrared emission pipe 12 and infrared ray receiver tube 13 are installed respectively in square pipe transmission cabin 1 two diagonal departments, infrared emission pipe 12 and infrared ray receiver tube 13 all are provided with 4, infrared emission pipe 12 and infrared ray receiver tube 13 are equidistant distribution, adopt infrared emission pipe 12 and infrared ray receiver tube 13 to survey, and the accuracy is high to two diagonal departments of installing square pipe transmission cabin 1 can avoid being strikeed. Follow 7 backs of board and be provided with silica gel connecting strip 14, the silica gel connecting strip is the right angle form setting, 14 one sides of silica gel connecting strip and 7 bolted connection of follow board, 14 another sides of silica gel connecting strip and the slider bolted connection of first electronic guide rail 6, follow board 7 and the slider of first electronic guide rail 6 pass through silica gel connecting strip 14 and connect, and when follow board 7 clashed into unmanned aerial vehicle, silica gel connecting strip 14 can absorb and the impact of dispersion through the bending, prevents that unmanned aerial vehicle from being damaged by the collision. Follow board 7 is the cavity setting, follow board 7 openly is provided with thermal-insulated ceramic plate 15, follow board 7 and thermal-insulated ceramic plate 15 mortise-tenon joint, follow board 7 has adopted hollow design, can the first electronic guide rail 6's of effectual reduction burden, and weight is light moreover. 3 bottom surfaces of electric turntable are provided with vacuum chuck (not shown), vacuum chuck and 3 threaded connection of electric turntable, vacuum chuck is provided with 10, vacuum chuck is the annular array and distributes, through being provided with vacuum chuck in 3 bottom surfaces of electric turntable, can the person of facilitating the use be connected with the car. Be provided with buffering elasticity cloth 16 on the direction mouth 8, 16 both ends of buffering elasticity cloth all with 1 riveting in square pipe launch cabin, buffering elasticity cloth 16 is mutually perpendicular with ball row 9, through be provided with buffering elasticity cloth 16 on direction mouth 8, unmanned aerial vehicle's wing directly strikes square pipe launch cabin 1 when can preventing to put into unmanned aerial vehicle. The extension section 2 is connected with the slider bolt of the second electric guide rail, and the extension section is convenient to disassemble and assemble with the slider of the second electric guide rail and is reliable in connection. Through being provided with the condition that electronic revolving stage 3 and barrier sensor 5 cooperation PLC4 can effectual detection external barrier under the on-vehicle condition, the departure angle of real-time adjustment unmanned aerial vehicle prevents that unmanned aerial vehicle from striking the barrier after the departure, and very suitable use under the on-vehicle condition can satisfy the vehicle and take off under the condition of traveling, and degree of automation is high moreover.
The beneficial effect of this embodiment does: through being provided with the condition that electric turntable and obstacle sensor cooperation PLC can effectual detection external obstacle under the on-vehicle condition, the departure angle of real-time adjustment unmanned aerial vehicle prevents that unmanned aerial vehicle from striking the obstacle after the departure, very be fit for using under on-vehicle condition, can satisfy the vehicle and take off under the condition of traveling, and degree of automation is high, in addition, be provided with electric telescopic handle between electric turntable and the square pipe launch cabin, the electric telescopic handle both ends are connected with electric turntable and square pipe launch cabin are articulated respectively, electric telescopic handle and PLC electric connection, PLC can drive electric telescopic handle and adjust the gradient in square pipe launch cabin. Unmanned aerial vehicle position detecting device includes infrared emission pipe and infrared ray receiver tube, infrared emission pipe and infrared ray receiver tube are in the face of setting, infrared emission pipe and infrared ray receiver tube are installed respectively in two diagonal departments in square pipe transmission cabin, infrared emission pipe and infrared ray receiver tube all are provided with more than one, infrared emission pipe and infrared ray receiver tube are equidistant distribution, adopt infrared emission pipe and infrared ray receiver tube to survey, the accuracy is high, and install two diagonal departments in square pipe transmission cabin and can avoid being strikeed. Follow the board back and be provided with the silica gel connecting strip, the silica gel connecting strip is the right angle form setting, silica gel connecting strip one side and follow board bolted connection, silica gel connecting strip another side and the slider bolted connection of first electronic guide rail, follow the board and pass through the silica gel connecting strip with the slider of first electronic guide rail and be connected, when the follow board strikes unmanned aerial vehicle, the silica gel connecting strip can absorb the impact with the dispersion through the bending, prevent that unmanned aerial vehicle from being damaged. Follow the board and be the cavity setting, follow the board and be provided with thermal-insulated ceramic plate on the front, follow board and thermal-insulated ceramic plate mortise-tenon joint, follow the board and adopted hollow design, the burden that can the first electronic guide rail of effectual reduction, weight is light moreover. The bottom surface of the electric turntable is provided with more than one vacuum sucker, the vacuum suckers are in threaded connection with the electric turntable and distributed in an annular array, and the vacuum suckers are arranged on the bottom surface of the electric turntable, so that a user can conveniently connect with an automobile. Be provided with buffering elasticity cloth on the guide way, buffering elasticity cloth both ends all with square pipe launch cabin riveting, buffering elasticity cloth is arranged mutually perpendicularly with the ball, through be provided with buffering elasticity cloth on the guide way, unmanned aerial vehicle's wing directly strikes square pipe launch cabin when can preventing to put into unmanned aerial vehicle. The extension section is connected with the slider bolt of the second electric guide rail, and the extension section is convenient to disassemble and assemble with the slider of the second electric guide rail and is reliable in connection.
Another technical problem to be solved by the present invention is to provide a control method for a vehicle-mounted unmanned aerial vehicle control system, which is characterized by comprising the following steps:
1) the PLC starts the unmanned aerial vehicle position detection device and the obstacle sensor for detection immediately after receiving a takeoff preparation signal sent by the terminal;
2) when the obstacle sensor detects that an obstacle exists in 30 meters, a signal is fed back to the PLC, and the PLC controls the electric rotary table to adjust the direction of the square tube launching cabin until no obstacle exists in 30 meters;
3) the PLC drives the second electric guide rail to unfold the extension section and then feeds a takeoff enabling signal back to the terminal;
4) starting the pulse jet unmanned aerial vehicle;
5) once the detection device detects that the pulse jet unmanned aerial vehicle moves in the square tube launching cabin, the signal is fed back to the PLC, the PLC drives the first electric guide rail to enable the following plate to follow the pulse jet unmanned aerial vehicle, and the pulse jet unmanned aerial vehicle can obtain good reaction force when taking off in the square tube launching cabin;
5) after the first electric guide rail reaches the maximum stroke, a signal is fed back to the PLC, and the PLC controls the first electric guide rail and the first electric guide rail to reset and stops the unmanned aerial vehicle position detection device and the obstacle sensor to work.
The above description is only an embodiment of the present invention, but the scope of the present invention is not limited thereto, and any changes or substitutions that are not thought of through the inventive work should be included in the scope of the present invention.
Claims (6)
1. The utility model provides an on-vehicle unmanned aerial vehicle control system which characterized in that: the square pipe launching cabin comprises a square pipe launching cabin, an extension section, an electric rotary table, a PLC (programmable logic controller) and a terminal, wherein the head end of the square pipe launching cabin is hinged with the electric rotary table, an unmanned aerial vehicle position detection device is arranged in the square pipe launching cabin, an obstacle sensor is arranged at the tail end of the square pipe launching cabin, a first electric guide rail is inlaid on the inner bottom surface of the square pipe launching cabin, a second electric guide rail is inlaid on the outer bottom surface of the square pipe launching cabin, a following plate is arranged on the first electric guide rail, guide ports matched with wings of the unmanned aerial vehicle are formed in the left side wall and the right side wall of the square pipe launching cabin, a ball row is arranged on each guide port, a dovetail groove is formed in the outer bottom surface of the square pipe launching cabin, a dovetail matched with the dovetail groove is arranged on the extension section, the dovetail groove is inserted into the, the extension section is linked with the second electric guide rail, the electric rotary table, the unmanned aerial vehicle position detection device, the first electric guide rail and the second electric guide rail are electrically connected with the PLC, and the terminal is in data connection with the PLC;
an electric telescopic rod is arranged between the electric rotary table and the square tube launching cabin, and two ends of the electric telescopic rod are respectively hinged with the electric rotary table and the square tube launching cabin;
follow the board back and be provided with the silica gel connecting strip, the silica gel connecting strip is the right angle form setting, silica gel connecting strip one side and follow board bolted connection, silica gel connecting strip another side and the slider bolted connection of first electronic guide rail.
2. The vehicle-mounted unmanned aerial vehicle control system of claim 1, wherein: the follow-up plate is the cavity setting, follow the board front side and be provided with thermal-insulated ceramic plate, follow board and thermal-insulated ceramic plate mortise-tenon joint.
3. The vehicle-mounted unmanned aerial vehicle control system of claim 2, wherein: the bottom surface of the electric turntable is provided with more than one vacuum sucker, the vacuum suckers are in threaded connection with the electric turntable and are distributed in an annular array.
4. The vehicle-mounted unmanned aerial vehicle control system of claim 3, wherein: the ball bearing device is characterized in that buffering elastic cloth is arranged on the guide opening, two ends of the buffering elastic cloth are riveted with the square tube launching cabin, and the buffering elastic cloth is perpendicular to the ball bearing row.
5. The vehicle-mounted unmanned aerial vehicle control system of claim 4, wherein: the extension section is connected with a slider bolt of the second electric guide rail.
6. The control method of the vehicle-mounted unmanned aerial vehicle control system according to claim 1, characterized by comprising the steps of:
1) the PLC starts the unmanned aerial vehicle position detection device and the obstacle sensor for detection immediately after receiving a takeoff preparation signal sent by the terminal;
2) when the obstacle sensor detects that an obstacle exists in 20-40 meters, a signal is fed back to the PLC, and the PLC controls the electric rotary table to adjust the direction of the square tube launching cabin until no obstacle exists in 20-40 meters;
3) the PLC drives the second electric guide rail to unfold the extension section and then feeds a takeoff enabling signal back to the terminal;
4) starting the pulse jet unmanned aerial vehicle;
5) once the detection device detects that the pulse jet unmanned aerial vehicle moves in the square tube launching cabin, the signal is fed back to the PLC, the PLC drives the first electric guide rail to enable the following plate to follow the pulse jet unmanned aerial vehicle, and the pulse jet unmanned aerial vehicle can obtain good reaction force when taking off in the square tube launching cabin;
6) after the first electric guide rail reaches the maximum stroke, a signal is fed back to the PLC, and the PLC controls the first electric guide rail and the first electric guide rail to reset and stops the unmanned aerial vehicle position detection device and the obstacle sensor to work.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201910813589.XA CN110654560B (en) | 2017-10-13 | 2017-10-13 | Vehicle-mounted unmanned aerial vehicle control system and control method thereof |
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| CN201910813589.XA CN110654560B (en) | 2017-10-13 | 2017-10-13 | Vehicle-mounted unmanned aerial vehicle control system and control method thereof |
| CN201710950995.1A CN107813958B (en) | 2017-10-13 | 2017-10-13 | A kind of vehicle-mounted unmanned aerial vehicle control system and its control method |
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| WO2022193079A1 (en) * | 2021-03-15 | 2022-09-22 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle system, and control method and apparatus for unmanned aerial vehicle |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
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Also Published As
| Publication number | Publication date |
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| CN110654560B (en) | 2021-04-23 |
| CN107813958B (en) | 2019-08-02 |
| CN107813958A (en) | 2018-03-20 |
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