A quad-rotor unmanned aerial vehicle debugging platform

Abstract

The application relates to the technical field of unmanned aerial vehicle debugging, and discloses a quad-rotor unmanned aerial vehicle debugging platform, which comprises an H-shaped base, T-shaped supports are fixedly connected to the two ends of the upper surface of the H-shaped base, a bearing seat is fixedly connected to the top end of the T-shaped support, an optical shaft is rotationally connected to the inner surface of the bearing seat, a balance block is fixedly connected to the circumferential surface of the optical shaft, a conversion plate one is fixedly connected to the upper surface of the balance block, and an electric cylinder is slidingly connected to the upper surface of the H-shaped base. In the application, the optical shaft swings along the bearing seat shaft center, thereby limiting the unmanned aerial vehicle, completing pitch and roll debugging, placing the unmanned aerial vehicle on a conversion plate two, enabling the unmanned aerial vehicle to move in all directions through the conversion plate two and a holder after starting, making the debugging more comprehensive, extending the free end of the electric cylinder, driving the holder and the conversion plate two to ascend or descend, and then debugging the sensitivity of the unmanned aerial vehicle to vertical instructions and the stability of the unmanned aerial vehicle lifting.

Description

Technical Field

[0001] This invention relates to the field of unmanned aerial vehicle (UAV) debugging technology, specifically a quadcopter UAV debugging platform. Background Technology

[0002] In the development of quadcopter drones, software and hardware integration and parameter tuning are key steps. Traditional methods of direct test flights are risky, inefficient, and difficult to collect data. They are also prone to crashes and damage due to loss of control. Dedicated debugging platforms use physical locking mechanisms to constrain the drone in a safe space, enabling it to operate at full power to simulate real flight conditions. At the same time, it allows engineers to safely and conveniently perform algorithm verification, parameter optimization, and sensor calibration, and enables real-time monitoring and analysis of flight data.

[0003] Patent CN223521052U discloses a quadcopter drone debugging platform. This patent includes a base with two fixed blocks fixedly connected to the top. Each fixed block has a fixed rod fixedly connected to its top, and a connecting rod is fixedly connected to the inner wall of the top of both fixed rods. A fixed seat is rotatably connected to the outer surface of the connecting rod. A support assembly is provided above the base. Specifically, by activating a motor, a support plate slides upwards on the corresponding fixed block's outer surface to support the fixed seat, eliminating the need for manual assistance. This not only frees workers from this tedious task, reducing labor costs, but also prevents unexpected drone start-up that could injure workers. However, while this patent solves these problems, it still suffers from issues such as power transmission during drone debugging causing platform swaying, resulting in unstable and inaccurate debugging processes. Furthermore, it lacks effective protection in case of drone loss of control, potentially causing safety problems. Additionally, it does not simulate outdoor wind conditions, limiting the usability of the debugged drone. Therefore, this patent proposes a quadcopter drone debugging platform to address these issues. Summary of the Invention

[0004] The technical problem to be solved by the present invention is to provide a quadcopter drone debugging platform to address the shortcomings of the prior art.

[0005] To solve the above-mentioned technical problems, the technical solution adopted by the present invention is: a quadcopter unmanned aerial vehicle (UAV) debugging platform, comprising: The H-shaped base has T-shaped brackets fixedly connected to both ends of its upper surface, a bearing seat fixedly connected to the top of the T-shaped brackets, an optical axis rotatably connected to the inner surface of the bearing seat, a balance block fixedly connected to the circumferential surface of the optical axis, a conversion plate fixedly connected to the upper surface of the balance block, and an electric cylinder slidably connected to the upper surface of the H-shaped base. A protective device is installed on the front and rear sides of the H-shaped base. The protective device is used to prevent the drone from falling out of control or being ejected in all directions. A simulation device is mounted on the protective device. The simulation device is used to simulate the impact of outdoor wind on the drone, making the debugging more accurate.

[0006] As a further technical solution, the H-shaped base includes: A gimbal, the gimbal being fixedly connected to the free end of the top of the electric cylinder, and a conversion plate being fixedly connected to the top of the gimbal; A copper column is fixedly connected to the upper surface of the conversion plate two, and the copper column is used to fix the drone.

[0007] As a further technical solution, the H-shaped base also includes: A damping rod is fixedly connected to the bottom of the T-shaped bracket on the side near the electric cylinder, and a force-dissipating seat is fixedly connected to the end of the damping rod near the electric cylinder. A stop rod is hinged to the upper surface of the stress-relieving seat, and a support rod is hinged to the side surface of the stress-relieving seat; A movable shaft, which is slidably connected to both sides of the electric cylinder; Side rods are fixedly connected to both sides of the circumferential surface of the gimbal.

[0008] As a further technical solution, the copper column and the upper surface of the conversion plate are fixedly connected, the upper surface of the force-dissipating seat and the H-shaped base are slidably connected, the bottom end of the support rod and the two sides of the bottom of the electric cylinder are hinged, and the top end of the movable shaft and the push rod are hinged.

[0009] As a further technical solution, the protective device includes: A lifting platform is slidably connected to the outer surface of a T-shaped bracket, and connecting plates are fixedly connected to the front and rear sides of the lifting platform. An inclined baffle is fixedly connected to the side of the connecting plate away from the lifting platform, and an observation window is fixedly connected to the inner surface of the inclined baffle.

[0010] As a further technical solution, the protective device also includes: A positive baffle is snapped onto the side of the inclined baffle away from the connecting plate, and a bottom plate is hinged to the bottom end of the positive baffle; A side slope plate is fixedly connected to the end of the side rod away from the gimbal, and a clip frame is fixedly connected to the end of the side slope plate near the T-shaped bracket.

[0011] As a further technical solution, the observation window is fixedly connected to the inner surface of the positive baffle, the bottom plate is fixedly connected to the lower surface of the inclined baffle, and the lifting platform is snapped into the inner surface of the frame.

[0012] As a further technical solution, the simulation device includes: A simulated fan is installed on both the front and rear sides of the conversion plate 2, and a telescopic cylinder is hinged to the lower surface of the simulated fan. An electric guide rail is fixedly connected to the upper surface of a base plate. A movable seat is fixedly connected to the moving end of the electric guide rail, and a rotating seat is fixedly connected to the upper surface of the movable seat.

[0013] As a further technical solution, the simulation device also includes: A sleeve shaft is fixedly connected to the bottom end of the telescopic cylinder. A retaining shaft is engaged on the inner surface of the sleeve shaft, and a shaft key is fixedly connected to the circumferential surface of the retaining shaft. A connector is fixedly connected to the upper surface of the rotating seat, and a positioning rod is slidably connected to the inner surface of the connector.

[0014] As a further technical solution, the retaining shaft is fixedly connected to the upper surface of the rotating seat, the inner surface of the sleeve shaft is provided with a keyway, and the keyway is engaged with the shaft key. The bottom end of the sleeve shaft abuts against the upper surface of the rotating seat. A through hole is provided on both sides of the circumferential surface of the sleeve shaft, and the through hole is engaged with the circumferential surface of the positioning rod. A through hole is provided on the inner side of the retaining shaft, and the through hole is engaged with the circumferential surface of the positioning rod. A spring is provided between the right side of the left end of the positioning rod and the connecting piece.

[0015] The present invention, by adopting the above technical solution, can bring the following beneficial effects: 1. This quadcopter drone debugging platform uses an optical axis that swings along the bearing seat axis to limit the drone's movement, enabling pitch and roll adjustments. The drone is placed on the second conversion plate, and after startup, it can move omnidirectionally via the conversion plate and gimbal, allowing for more comprehensive debugging. The free end of the electric cylinder extends, causing the gimbal and conversion plate to rise or fall, thereby adjusting the drone's sensitivity to vertical commands and the stability of its ascent and descent. The electric cylinder, affected by the vertical movement, slides left and right on the H-shaped base, reducing the swaying force and ensuring debugging stability and data accuracy. When the electric cylinder shifts, it causes the stop rod and support rod to shift, and the stop rod causes the force-dissipating seat to slide on the H-shaped base. The force-dissipating seat then presses against the damping rod, further reducing the swaying force and promoting stability during the debugging process.

[0016] 2. The quadcopter drone debugging platform, with its obstruction and protection by the inclined baffle and the front baffle, can prevent the drone from detaching from the first or second conversion plate due to excessive force and being thrown outwards, thus improving the operational safety of the device. Rotating to open the front baffle allows the drone to be separated from the inclined baffle, at which point it can be quickly disassembled and installed, improving the ease of use of the device.

[0017] 3. In the quadcopter drone debugging platform, if the drone falls out of control, it will be supported by the base plate, preventing the drone from falling directly to the ground and causing damage. The lifting platform lifts the base plate and inclined baffle through the connecting plate, and the base plate then lifts the positive baffle, so that the device moves synchronously with the drone and always stays within the effective range of drone protection, thus improving the applicability of the device.

[0018] 4. The quadcopter drone debugging platform uses a telescopic cylinder to extend and retract, thereby moving the simulated fan up and down. This allows the simulated fan to move to the upper and lower sides of the drone, simulating different wind directions and improving the simulation effect. Adjusting the angle of the simulated fan increases the breadth of simulated wind directions. Moving the simulated fan away from or closer to the drone from the left and right sides increases the simulation range, further enhancing the simulation effect of the device and the sample breadth of the debugging data.

[0019] 5. The quadcopter UAV debugging platform, after the key and keyway are connected, allows the rotating seat to easily disassemble and install the simulated fan while driving it to rotate, facilitating maintenance and ensuring simulation effect. The positioning rod is inserted into the locking hole between the sleeve shaft and the retaining shaft to lock them, thereby locking the telescopic cylinder and the simulated fan. After the positioning rod is pulled out of the sleeve shaft, the simulated fan can be quickly disassembled, improving the installation stability of the simulated fan, ensuring simulation accuracy, and promoting disassembly convenience. Attached Figure Description

[0020] Figure 1 This is a schematic diagram of the overall three-dimensional structure of the present invention; Figure 2 This is a three-dimensional half-section diagram of the front side of the conversion plate 2 of the present invention; Figure 3 For the present invention Figure 2 A magnified structural diagram of A in the middle; Figure 4 This is a three-dimensional half-sectional view of the front side of the protective device of the present invention; Figure 5 For the present invention Figure 4 A magnified structural diagram of B in the diagram; Figure 6 This is a three-dimensional half-section diagram of the front side of the simulation device of the present invention; Figure 7 For the present invention Figure 6 A magnified structural diagram of C; Figure 8 For the present invention Figure 6 A magnified structural diagram of D in the diagram.

[0021] In the diagram: 1. H-shaped base; 2. T-shaped bracket; 3. Bearing seat; 4. Optical axis; 5. Balance block; 6. Conversion plate one; 7. Electric cylinder; 8. Protective device; 9. Simulation device; 10. Gimbal; 11. Conversion plate two; 12. Copper column; 13. Damping rod; 14. Stress-relieving seat; 15. Support rod; 16. Movable shaft; 17. Support rod; 18. Side rod; 81. Lifting platform; 82. Connecting plate; 83. Inclined baffle; 84. Observation window; 85. Front baffle; 86. Base plate; 87. Side inclined plate; 88. Clip frame; 91. Simulated fan; 92. Telescopic cylinder; 93. Electric guide rail; 94. Moving seat; 95. Rotating seat; 96. Sleeve shaft; 97. Clip shaft; 98. Shaft key; 99. Connecting piece; 910. Positioning rod. Detailed Implementation

[0022] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0023] Please see Figures 1-8One embodiment of the present invention is as follows: a quadcopter drone debugging platform, including an H-shaped base 1, T-shaped brackets 2 fixedly connected to both ends of the upper surface of the H-shaped base 1, a bearing seat 3 fixedly connected to the top of the T-shaped brackets 2, an optical axis 4 rotatably connected to the inner surface of the bearing seat 3, a balance block 5 fixedly connected to the circumferential surface of the optical axis 4, a conversion plate 6 fixedly connected to the upper surface of the balance block 5, an electric cylinder 7 slidably connected to the upper surface of the H-shaped base 1, a protective device 8 disposed on the front and rear sides of the H-shaped base 1, the protective device 8 being used to prevent the drone from losing control and falling or popping out in all directions, and a simulation device 9 disposed on the protective device. On 8, the simulation device 9 is used to simulate the impact of outdoor wind on the drone, making the debugging more precise. The optical axis 4 swings along the axis of the bearing seat 3, thereby limiting the drone and completing pitch and roll debugging. The drone is placed on the conversion plate 2 11. After the drone is started, it can move omnidirectionally through the conversion plate 2 11 and the gimbal 10, making the debugging more comprehensive. The free end of the electric cylinder 7 extends, driving the gimbal 10 and the conversion plate 2 11 to rise or fall, thereby debugging the drone's sensitivity to vertical command response and the stability of the drone's ascent and descent. The H-shaped base 1 includes the gimbal 10, which is fixedly connected to the... The top free end of the electric cylinder 7 and the top of the gimbal 10 are fixedly connected to a conversion plate 11. A copper column 12 is fixedly connected to the upper surface of the conversion plate 11 and is used to fix the drone. The H-shaped base 1 also includes a damping rod 13, which is fixedly connected to the bottom of the T-shaped bracket 2 near the electric cylinder 7. A force-dissipating seat 14 is fixedly connected to the end of the damping rod 13 near the electric cylinder 7. A stop rod 15 is hinged to the upper surface of the force-dissipating seat 14. A support rod 17 is hinged to the side surface of the force-dissipating seat 14. A movable shaft 16 is slidably connected to both sides of the electric cylinder 7. A side rod 18 is fixedly connected to both sides of the circumferential surface of the gimbal 10. The upper surface of the conversion plate 12 is fixedly connected to the upper surface of the conversion plate 6, the upper surface of the force-dissipating seat 14 is slidably connected to the upper surface of the H-shaped base 1, the bottom end of the support rod 17 is hinged to both sides of the bottom of the electric cylinder 7, and the top end of the movable shaft 16 is hinged to the top end of the push rod 15. The electric cylinder 7 is affected and slides left and right on the H-shaped base 1 to reduce the shaking force, ensuring the stability of the debugging and the accuracy of the data. When the electric cylinder 7 shifts, it drives the push rod 15 and the support rod 17 to shift. The push rod 15 drives the force-dissipating seat 14 to slide on the H-shaped base 1. The force-dissipating seat 14 then squeezes the damping rod 13, further reducing the shaking force of the device and promoting the stability of the device during the debugging process.

[0024] Working principle: Place the drone on conversion plate 1 (6), securing its bottom to the copper pillar 12. Start and control the drone. After startup, conversion plate 1 (6) drives the balance block 5 and optical axis 4 to swing along the axis of bearing seat 3, thus limiting the drone's movement and completing pitch and roll adjustments. Place the drone on conversion plate 2 (11). After startup, the drone can move omnidirectionally via conversion plate 2 (11) and gimbal 10, allowing for more comprehensive adjustments. Activate electric cylinder 7; its free end extends, causing gimbal 10 and conversion plate 2 (11) to rise or fall, thereby adjusting the drone's response to vertical commands. Sensitivity and the smoothness of drone takeoff and landing are crucial. In general devices, if the drone's force is not properly controlled, the debugging components will shake due to the drone, resulting in inaccurate debugging data. During the use of this device, the force of the drone's movement is transmitted to the electric cylinder 7. The electric cylinder 7 is affected and slides left and right on the H-shaped base 1 to reduce the shaking force, ensuring debugging stability and data accuracy. When the electric cylinder 7 shifts, it drives the abutment rod 15 and the support rod 17 to shift. The abutment rod 15 drives the force-dissipating seat 14 to slide on the H-shaped base 1. The force-dissipating seat 14 then presses against the damping rod 13, further reducing the shaking force of the device and promoting the stability of the device during debugging.

[0025] Please see Figures 1-8 Based on the above embodiments, in another embodiment of the present invention, the protective device 8 includes a lifting platform 81, which is slidably connected to the outer surface of the T-shaped bracket 2. Connecting plates 82 and inclined baffles 83 are fixedly connected to the front and rear sides of the lifting platform 81. The inclined baffles 83 are fixedly connected to the side of the connecting plate 82 away from the lifting platform 81. An observation window 84 is fixedly connected to the inner surface of the inclined baffles 83. The obstruction and protection provided by the inclined baffles 83 and the positive baffle 85 can prevent the drone from detaching from the first conversion plate 6 or the second conversion plate 11 due to excessive force and falling outwards, causing harm to the debugging personnel, thereby improving the operational safety of the device. Rotating the positive baffle 85 opens it, disengaging it from the inclined baffles 83, allowing for quick disassembly and installation of the drone, improving the ease of use of the device. The protective device 8 also includes the positive baffle 85. The front baffle 85 is snapped onto the side of the inclined baffle 83 away from the connecting plate 82. The bottom end of the front baffle 85 is hinged to the base plate 86. The side inclined plate 87 is fixedly connected to the end of the side rod 18 away from the gimbal 10. The end of the side inclined plate 87 near the T-shaped bracket 2 is fixedly connected to the frame 88. The observation window 84 is fixedly connected to the inner surface of the front baffle 85. The base plate 86 is fixedly connected to the lower surface of the inclined baffle 83. The lifting platform 81 is snapped onto the inner surface of the frame 88. If the drone falls out of control, it will be stopped by the base plate 86, preventing the drone from falling directly to the ground and causing damage. The lifting platform 81 drives the base plate 86 and the inclined baffle 83 to rise through the connecting plate 82. The base plate 86 then drives the front baffle 85 to rise, thereby making the device move synchronously with the drone and always keeping it within the effective range of drone protection, thus improving the applicability of the device.

[0026] Working principle: During the debugging process of the drone, the obstruction and protection of the inclined baffle 83 and the positive baffle 85 can prevent the drone from detaching from the first conversion plate 6 or the second conversion plate 11 due to excessive force and falling outwards, thus improving the operational safety of the device. Furthermore, during debugging, the debugging personnel can observe the drone through the observation window 84. When it is necessary to load or unload the drone, rotate and open the positive baffle 85 to separate it from the inclined baffle 83, allowing for quick disassembly and installation of the drone, improving the ease of use of the device. If the drone falls uncontrollably, it will be stopped by the base plate 86. To prevent the drone from falling directly to the ground and causing damage, after the positive baffle 85 is closed, during the drone's lifting test, the free end of the electric cylinder 7 extends and drives the gimbal 10 to rise. The gimbal 10 drives the side rod 18 to rise, the side rod 18 drives the side inclined plate 87 to rise, the side inclined plate 87 drives the clamping frame 88 to rise, and the clamping frame 88 drives the lifting platform 81 to slide and rise on the surface of the T-shaped bracket 2. The lifting platform 81 drives the base plate 86 and the inclined baffle 83 to rise through the connecting plate 82. The base plate 86 then drives the positive baffle 85 to rise, thereby making the device move synchronously with the drone and always stay within the effective range of drone protection, thus improving the applicability of the device.

[0027] Please see Figures 1-8Based on the above embodiments, in another embodiment of the present invention, the simulation device 9 includes a simulation fan 91, which is disposed on the front and rear sides of the conversion plate 11. A telescopic cylinder 92 is hinged to the lower surface of the simulation fan 91. An electric guide rail 93 is fixedly connected to the upper surface of the base plate 86. A movable seat 94 is fixedly connected to the moving end of the electric guide rail 93. A rotating seat 95 is fixedly connected to the upper surface of the movable seat 94. The telescopic cylinder 92 extends and retracts vertically, thereby driving the simulation fan 91 to move vertically, so that the simulation fan 91 can move to the top of the drone. Different wind directions are simulated on both sides, improving the simulation effect. Adjusting the angle of the simulated fan 91 increases the breadth of simulated wind directions. Moving the simulated fan 91 away from or towards the drone from the left and right sides increases the simulation range, further improving the simulation effect of the device and the sample breadth of the debugging data. The simulation device 9 also includes a sleeve shaft 96, which is fixedly connected to the bottom end of the telescopic cylinder 92. A retaining shaft 97 is snapped onto the inner surface of the sleeve shaft 96, and a key 98 is fixedly connected to the circumferential surface of the retaining shaft 97. A connecting piece 99 is fixedly connected to the rotating seat 95. On the upper surface, a positioning rod 910 is slidably connected to the inner surface of the connector 99. A retaining shaft 97 is fixedly connected to the upper surface of the rotating seat 95. A keyway is provided on the inner surface of the sleeve shaft 96, and the keyway engages with the shaft key 98. The bottom end of the sleeve shaft 96 abuts against the upper surface of the rotating seat 95. Through holes are provided on both sides of the circumferential surface of the sleeve shaft 96, and the through holes engage with the circumferential surface of the positioning rod 910. A second through hole is provided on the inner side of the retaining shaft 97, and the second through hole engages with the circumferential surface of the positioning rod 910. A space is provided between the left end and the right side of the positioning rod 910 and the connector 99. With the spring, the key 98 and the keyway are connected, allowing the rotating seat 95 to easily disassemble and install the simulated fan 91 while driving it to rotate. This facilitates maintenance, ensures the simulation effect, and the positioning rod 910 is inserted into the locking hole between the sleeve shaft 96 and the retaining shaft 97 to lock them together. This locks the telescopic cylinder 92 and the simulated fan 91. After the positioning rod 910 is pulled out of the sleeve shaft 96, the simulated fan 91 can be quickly disassembled, improving the installation stability of the simulated fan 91, ensuring simulation accuracy, and promoting ease of disassembly.

[0028] Working Principle: Activating the simulated fan 91 simulates the ambient wind conditions when the drone is used outdoors, making the testing environment more realistic and improving the accuracy of the testing data. Activating the telescopic cylinder 92 causes it to extend and retract, thus moving the simulated fan 91 up and down, allowing it to move to the upper and lower sides of the drone to simulate different wind directions and improve the simulation effect. Activating the rotating base 95 causes the telescopic cylinder 92 and the simulated fan 91 to rotate, thereby adjusting the angle of the simulated fan 91 and increasing the range of simulated wind directions. Simultaneously, activating the electric guide rail 93 causes the moving base 94 to move left and right. The moving base 94, in turn, moves the simulated fan 91 left and right via the rotating base 95 and the telescopic cylinder 92, moving the simulated fan 91 away from or closer to the drone from the left and right sides, increasing the simulation range and further improving the simulation performance. The simulation effect and the wide range of debugging data samples are optimized. The telescopic cylinder 92 is inserted into the retaining shaft 97 at the top of the rotating seat 95 through the sleeve shaft 96. The shaft key 98 fixed on the circumference of the retaining shaft 97 is connected to the keyway opened on the inner side of the sleeve shaft 96. With the rotating seat 95 able to drive the simulated fan 91 to rotate, it is easy to disassemble and install the simulated fan 91, which facilitates its maintenance and ensures the simulation effect. After the retaining shaft 97 is inserted into the sleeve shaft 96, the positioning rod 910 slides to the right in the connector 99 under the influence of the spring force and inserts into the locking hole opened between the sleeve shaft 96 and the retaining shaft 97, locking the two together, and thus locking the telescopic cylinder 92 and the simulated fan 91. Conversely, the positioning rod 910 is pulled out of the sleeve shaft 96 and the retaining shaft 97, which allows for quick disassembly of the simulated fan 91. This improves the stability of the simulated fan 91 during installation, ensures the simulation accuracy, and facilitates disassembly.

[0029] This invention provides a quadcopter unmanned aerial vehicle (UAV) debugging platform. Many methods and approaches exist for implementing this technical solution; the above description is merely a preferred embodiment. It should be noted that those skilled in the art can make various improvements and modifications without departing from the principles of this invention, and these improvements and modifications should also be considered within the scope of protection of this invention. All components not explicitly stated in this embodiment can be implemented using existing technologies.

Claims

1. A quadcopter unmanned aerial vehicle (UAV) debugging platform, characterized in that, include: H-shaped base (1), T-shaped brackets (2) are fixedly connected to both ends of the upper surface of the H-shaped base (1), bearing seat (3) is fixedly connected to the top of the T-shaped bracket (2), optical axis (4) is rotatably connected to the inner surface of the bearing seat (3), balance block (5) is fixedly connected to the circumferential surface of the optical axis (4), conversion plate (6) is fixedly connected to the upper surface of the balance block (5), and electric cylinder (7) is slidably connected to the upper surface of the H-shaped base (1). Protective device (8), the protective device (8) is set on the front and rear sides of the H-shaped base (1), the protective device (8) is used to prevent the drone from falling out of control or being ejected in all directions; The simulation device (9) is installed on the protective device (8). The simulation device (9) is used to simulate the impact of outdoor wind on the drone, so as to make the debugging more accurate.

2. The quadcopter UAV debugging platform according to claim 1, characterized in that: The H-shaped base (1) includes: The gimbal (10) is fixedly connected to the top free end of the electric cylinder (7), and the top of the gimbal (10) is fixedly connected to the conversion plate (11). A copper column (12) is fixedly connected to the upper surface of the conversion plate (11) and is used to fix the drone.

3. The quadcopter UAV debugging platform according to claim 2, characterized in that: The H-shaped base (1) also includes: Damping rod (13), the damping rod (13) is fixedly connected to the bottom of the T-shaped bracket (2) on the side near the electric cylinder (7), and the end of the damping rod (13) near the electric cylinder (7) is fixedly connected to a force-dissipating seat (14). A stop rod (15) is hinged to the upper surface of a stress-relieving seat (14), and a support rod (17) is hinged to the side surface of the stress-relieving seat (14). Movable shaft (16), which is slidably connected to both sides of electric cylinder (7); Side rod (18) is fixedly connected to both sides of the circumferential surface of the gimbal (10).

4. The quadcopter UAV debugging platform according to claim 3, characterized in that: The copper column (12) and the upper surface of the conversion plate (6) are fixedly connected, the upper surface of the force-dissipating seat (14) and the upper surface of the H-shaped base (1) are slidably connected, the bottom end of the support rod (17) and the bottom sides of the electric cylinder (7) are hinged, and the top end of the movable shaft (16) and the abutment rod (15) are hinged.

5. A quadcopter UAV debugging platform according to claim 4, characterized in that: The protective device (8) includes: The lifting platform (81) is slidably connected to the outer surface of the T-shaped bracket (2), and the front and rear sides of the lifting platform (81) are fixedly connected with connecting plates (82). An inclined baffle (83) is fixedly connected to the side of the connecting plate (82) away from the lifting platform (81), and an observation window (84) is fixedly connected to the inner surface of the inclined baffle (83).

6. A quadcopter UAV debugging platform according to claim 5, characterized in that: The protective device (8) also includes: A positive baffle (85) is snapped onto the side of the inclined baffle (83) away from the connecting plate (82), and a bottom plate (86) is hinged to the bottom end of the positive baffle (85). Side plate (87), the side plate (87) is fixedly connected to the end of the side rod (18) away from the gimbal (10), and the end of the side plate (87) near the T-shaped bracket (2) is fixedly connected to a clip frame (88).

7. A quadcopter UAV debugging platform according to claim 6, characterized in that: The observation window (84) and the inner surface of the positive baffle (85) are fixedly connected, the bottom plate (86) and the lower surface of the inclined baffle (83) are fixedly connected, and the lifting platform (81) and the inner surface of the frame (88) are snapped together.

8. A quadcopter UAV debugging platform according to claim 7, characterized in that: The simulation device (9) includes: A simulated fan (91) is installed on the front and rear sides of the conversion plate two (11), and a telescopic cylinder (92) is hinged to the lower surface of the simulated fan (91). An electric guide rail (93) is fixedly connected to the upper surface of the base plate (86). A movable seat (94) is fixedly connected to the moving end of the electric guide rail (93). A rotating seat (95) is fixedly connected to the upper surface of the movable seat (94).

9. A quadcopter UAV debugging platform according to claim 8, characterized in that: The simulation device (9) further includes: A sleeve shaft (96) is fixedly connected to the bottom end of the telescopic cylinder (92). A retaining shaft (97) is snapped onto the inner surface of the sleeve shaft (96). A shaft key (98) is fixedly connected to the circumferential surface of the retaining shaft (97). A connector (99) is fixedly connected to the upper surface of the rotating seat (95), and a positioning rod (910) is slidably connected to the inner surface of the connector (99).

10. A quadcopter UAV debugging platform according to claim 9, characterized in that: The retaining shaft (97) is fixedly connected to the upper surface of the rotating seat (95). The inner surface of the sleeve shaft (96) is provided with a keyway, and the keyway is engaged with the shaft key (98). The bottom end of the sleeve shaft (96) abuts against the upper surface of the rotating seat (95). The two sides of the circumferential surface of the sleeve shaft (96) are provided with a through hole, and the through hole is engaged with the circumferential surface of the positioning rod (910). The inner side of the retaining shaft (97) is provided with a through hole, and the through hole is engaged with the circumferential surface of the positioning rod (910). A spring is provided between the right side of the left end of the positioning rod (910) and the connecting piece (99).

Images