Lighting system for tethered hovering platform
By designing a lighting system including a lamp set device and a flight control system, the problem of uneven light spots in the prior art is solved, and a completely bright illuminated light spot is achieved, and the detection efficiency is improved.
Patent Information
- Application Number
- CN202210473911.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2022-04-29
- Publication Date
- 2025-02-18
- Estimated Expiration
- 2042-04-29
AI Technical Summary
The existing tethered drone lighting system is uneven when operating at night, resulting in a reduced detection efficiency and the inability to achieve a completely bright illuminated spot.
A lighting system including a light group device and a flight control system is designed. The light group device is composed of an adjustment mechanism and a lighting mechanism. The flight control system calculates the effective area through the processor, a light spot control module, a height control module and an angle control module. Compensation is performed through the spot recognition module and the spot compensation module to ensure the complete brightness of the spot.
The complete brightness of the light spot is achieved, the lighting efficiency is improved, and the effective detection capability is ensured during night operation.
Smart Images

Figure CN114919769B_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the technical field of tethered aircraft, and more particularly to a lighting system applied to a tethered hovering platform. Background Art
[0002] A tethered drone is a special form of multi-rotor drone. It uses ground power transmitted by tethered cables as its power source, replacing traditional lithium batteries as the power source of the drone. Tethered drones have the ability to hover for a long time and can be deployed quickly, so they are widely used in various industries.
[0003] At present, due to the wide application of drones, drones are used for detection in situations where humans cannot reach or are inconvenient to handle, so as to detect areas that need to be detected. In many cases, drones need to work at night. When working at night, the existing lighting system will be configured on the tethered drone. The existing lighting system will power the lighting system through the tethered base station, and the lighting angle and lighting brightness of the lighting system will be controlled by the control mechanism. However, in actual applications, this method has the problem that the illuminated light spot is elliptical or nearly circular, and the light spot is usually brighter in the middle area than in the periphery, and the light spot cannot be completely bright. The effective lighting light spot is only 40% to 60%, and the light spot illumination is extremely uneven, resulting in the need to control the drone to move gradually to illuminate the area that is not fully illuminated during detection. This method reduces the detection efficiency. Summary of the invention
[0004] In view of the deficiencies in the prior art, an object of the present invention is to provide a lighting system for a tethered hovering platform, wherein the lighting system provides a completely bright illumination spot to improve the lighting efficiency.
[0005] To achieve the above object, the present invention provides the following technical solutions:
[0006] A lighting system for a tethered hovering platform, comprising:
[0007] A light assembly device, the light assembly device is arranged on the mooring platform, the light assembly device comprises an adjustment mechanism and a lighting mechanism, the lighting mechanism comprises a plurality of lighting lamps for providing lighting, the lighting mechanism is connected to the adjustment mechanism, and the adjustment mechanism is used to adjust the illumination angle of the lighting mechanism;
[0008] A flight control system, the flight control system includes a processor, a light spot control module, a height control module and an angle control module, the light spot control module is configured with preset lighting information, the light spot control module is used to control the lighting of the lighting lamp providing illumination according to the lighting information, the lighting information represents the illumination angle of the lighting lamp, the height adjustment module is configured with preset height information, the height adjustment module is used to control and adjust the flight height of the tethered platform according to the height information, the height information represents the height of the tethered platform from the illumination surface, the angle control module is configured with preset offset information, the angle adjustment module is used to adjust the angle of the lighting mechanism according to the offset information, the offset information represents the offset inclination value of the lighting mechanism, the processor is configured with a light spot matching strategy and an area algorithm, the light spot matching strategy includes retrieving the lighting information, height information and offset information and calculating the effective area of the illumination light spot according to the area algorithm, the processor is also configured with a memory unit, the memory unit is used to store the lighting information, height information and offset information corresponding to the effective area;
[0009] The flight control system also includes a light spot compensation module and a light spot recognition module. The light spot recognition module is used to obtain the actual light spot area formed and generate the actual area. The light spot recognition module also obtains the actual height of the tethered platform to generate actual height data, and is also used to obtain the number and angle of the lit lighting lamps to generate actual lighting data and obtain actual offset data of the lighting mechanism. The light spot compensation module is configured with a compensation strategy, which includes retrieving the effective area and the actual area, and generating compensation data based on the comparison of the effective area and the actual area. The light group device adjusts the illumination mechanism and the adjustment mechanism based on the compensation data.
[0010] As a further improvement of the present invention, the lighting mechanism also includes a lamp rack and a lamp board, the lamp rack is connected to the mooring platform, a connecting shaft is provided on the lamp rack, the lamp board is rotatably connected to the connecting shaft, a plurality of lamp grooves are provided on the lamp board, and a lighting lamp is installed in any of the lamp grooves.
[0011] As a further improvement of the present invention, the adjusting mechanism includes an adjusting servo, an adjusting gear and a driven gear, the adjusting servo is connected to the lamp stand, the adjusting gear is coaxially fixedly connected to the adjusting servo, and the driven gear is connected to the lamp panel and meshes with the adjusting gear.
[0012] As a further improvement of the present invention, the lamp panels are arranged as two symmetrically arranged along the connecting axis, and adjustment mechanisms are respectively arranged at the ends of the two lamp panels facing away from each other, and the two adjustment mechanisms respectively control the tilting of the lamp panels along the axis of the connecting axis.
[0013] As a further improvement of the present invention, the area algorithm includes:
[0014] s=π[(tanx° / 2)*h] 2
[0015] Among them: s represents the effective area, x represents the lighting information, and h represents the height information.
[0016] As a further improvement of the present invention, the area algorithm further includes:
[0017] s=π{[tan(x°+y°) / 2]*h}[(tanx° / 2)*h]
[0018] Among them: s represents the effective area, and y represents the offset information.
[0019] As a further improvement of the present invention, the area algorithm further includes:
[0020] s=2π{[tan(x°+y°) / 2]*h}[tanx° / 2*h]*z
[0021] Among them: z represents the combination coefficient.
[0022] As a further improvement of the present invention, the area algorithm further includes:
[0023] s=π{[tan(x°+y°) / 2]*h}[(tanx° / 2)*h]*a*z
[0024] Among them: a represents the number of lights on.
[0025] As a further improvement of the present invention, the compensation strategy includes:
[0026] If the actual area is larger than the effective area, it is determined that one or more of the actual lighting data, the actual height data and the actual offset data exceeds the input lighting information, height information and offset information of the area algorithm when calculating the effective area. At this time, the compensation data includes the difference between the actual lighting data, the actual height data and the actual offset data and the lighting information, the height information and the offset information. The lamp group device is compensated and adjusted according to the compensation data.
[0027] If the actual area is smaller than the effective area, it is judged that one or more of the actual lighting data, actual height data and actual offset data are smaller than the lighting information, height information and offset information input by the area algorithm when calculating the effective area. At this time, the compensation data includes the difference between the actual lighting data, actual height data and actual offset data and the lighting information, height information and offset information. The lighting group device is compensated and adjusted according to the compensation data.
[0028] As a further improvement of the present invention, the flight control system further includes a compensation judgment module, and a judgment strategy is configured in the compensation judgment module, and the judgment strategy is specifically:
[0029] When the effective area is different from the actual area, determining the cause of the error and generating failure data and / or physical damage data, wherein the failure data indicates that the lighting lamp has experienced use failure, and the physical damage indicates that the lamp assembly device has experienced physical damage;
[0030] The flight control system generates maintenance data according to the exhaustion data and / or the physical damage data, wherein the maintenance data represents an area where a fault occurs and needs maintenance.
[0031] The beneficial effects of the present invention are as follows: the effective area corresponding to the lighting information, height information and offset information can be calculated through the spot matching strategy configured in the processor of the flight control system, and the actual area and the effective area are compared according to the spot recognition module and the spot compensation module. The light group device is adjusted by the compensation data generated by the compensation strategy to match the actual area with the effective area, thereby forming sufficient lighting, achieving the effect of providing a completely bright illumination spot and improving lighting efficiency. BRIEF DESCRIPTION OF THE DRAWINGS
[0032] Figure 1 This is a schematic diagram of a three-dimensional structure of a first form of a lamp assembly device in the present invention;
[0033] Figure 2 A schematic diagram of a first embodiment of the three-dimensional structure of the lamp assembly device of the present invention
[0034] Figure 3 It is a schematic diagram showing the structure of the lighting mechanism in the lamp assembly device.
[0035] Figure numerals: 1. lamp assembly; 2. adjusting mechanism; 21. adjusting servo; 22. adjusting gear; 23. driven gear; 3. lighting mechanism; 31. lamp holder; 32. lamp board; 33. connecting shaft; 4. lighting lamp. DETAILED DESCRIPTION
[0036] The present invention is further described in detail below in conjunction with the accompanying drawings and embodiments. The same parts are represented by the same reference numerals. It should be noted that the words "front", "rear", "left", "right", "upper" and "lower" used in the following description refer to directions in the accompanying drawings, and the words "bottom surface" and "top surface", "inner" and "outer" refer to directions toward or away from the geometric center of a specific component, respectively.
[0037] refer to Figures 1 to 3As shown, a specific embodiment of the lighting system applied to a moored hovering platform of the present invention comprises a light assembly device 1, which is arranged on the moored platform, and the light assembly device 1 comprises an adjustment mechanism 2 and a lighting mechanism 3, and the lighting mechanism 3 comprises a plurality of lighting lamps 4 for providing lighting, and the lighting mechanism 3 is connected to the adjustment mechanism 2, and the adjustment mechanism 2 is used to adjust the illumination angle of the lighting mechanism 3, and the lighting mechanism 3 also comprises a lamp holder 31 and a lamp board 32, and the lamp holder 31 is connected to the moored platform, and a connecting shaft 33 is arranged on the lamp holder 31, and the lamp board 32 is rotatably connected to the connecting shaft 33, and a plurality of lamp slots are provided on the lamp board 32, and a lighting lamp 4 is installed in any lamp slot The adjusting mechanism 2 includes an adjusting steering engine 21, an adjusting gear 22 and a driven gear 23. The adjusting steering engine 21 is connected to the lamp frame 31. The adjusting gear 22 is coaxially and fixedly connected to the adjusting steering engine 21. The driven gear 23 is connected to the lamp board 32 and meshes with the adjusting gear 22. The lamp board 32 is arranged as two symmetrically arranged along the connecting shaft 33. The adjusting mechanisms 2 are respectively arranged at the ends of the two lamp boards 32 which are away from each other. The two adjusting mechanisms 2 respectively control the tilting of the lamp boards 32 along the axis of the connecting shaft 33, so that when the lamp boards 32 are adjusted, the lamp boards 32 on both sides of the connecting shaft 33 are adjusted independently of each other, thereby achieving the ability to adjust different inclination angles.
[0038] It also includes a flight control system, which includes a processor, a light spot control module, a height control module and an angle control module. The light spot control module is configured with preset lighting information. The light spot control module is used to control the lighting of the lighting lamp 4 that provides illumination according to the lighting information. The lighting information represents the illumination angle of the lighting lamp 4. The height adjustment module is configured with preset height information. The height adjustment module is used to control and adjust the flight height of the tethered platform according to the height information. The height information represents the height of the tethered platform from the illumination surface. The angle control module is configured with preset offset information. The angle adjustment module is used to adjust the angle of the lighting mechanism 3 according to the offset information. The offset information represents the offset inclination value of the lighting mechanism 3. The processor is configured with a light spot matching strategy and an area algorithm. The light spot matching strategy includes retrieving the lighting information, height information and offset information and calculating the effective area of the illumination spot according to the area algorithm. The processor is also configured with a memory unit. The memory unit is used to store the lighting information, height information and offset information corresponding to the effective area. The flight control system also includes a spot compensation module and a spot recognition module. The spot recognition module is used to obtain the actual spot area formed and generate the actual area. The spot recognition module also obtains the actual height of the tethered platform to generate actual height data, and is also used to obtain the number and angle of the lit lighting lamps 4 to generate actual lighting data and obtain the actual offset data of the lighting mechanism 3. The spot compensation module is configured with a compensation strategy, which includes retrieving the effective area and the actual area, and generating compensation data based on the comparison of the effective area and the actual area. The lamp group device 1 adjusts the illumination mechanism and the adjustment mechanism 2 according to the compensation data.
[0039] The area algorithm includes when the effective area of lighting needs to be changed for single or multiple groups:
[0040] s=π[(tanx° / 2)*h] 2
[0041] Among them: s represents the effective area, x represents the lighting information, and h represents the height information, so that the size of the effective area can be calculated according to different heights and lighting information;
[0042] The area algorithm also includes calculations when expanding the effective spot. When calculating the effective area at a certain offset angle:
[0043] s=π{[tan(x°+y°) / 2]*h}[(tanx° / 2)*h]
[0044] Among them: s represents the effective area, y represents the offset information, so as to calculate the effective area;
[0045] The area algorithm also includes calculations when expanding the effective spot, when calculating the effective area of overlapping illumination after symmetrical offset:
[0046] s=2π{[tan(x°+y°) / 2]*h}[tanx° / 2*h]*z
[0047] Among them: z represents the combination coefficient, so that the effective area can be calculated;
[0048] The area algorithm also includes calculations when expanding the effective spot, when multiple groups of symmetrically offset and overlapping illumination are used for effective area calculations:
[0049] s=π{[tan(x°+y°) / 2]*h}[(tanx° / 2)*h]*a*z
[0050] Where: a represents the number of lights on, so as to calculate the effective area.
[0051] Compensation strategies include:
[0052] If the actual area is larger than the effective area, it is determined that one or more of the actual lighting data, the actual height data and the actual offset data exceeds the input lighting information, height information and offset information of the area algorithm when calculating the effective area. At this time, the compensation data includes the difference between the actual lighting data, the actual height data and the actual offset data and the lighting information, the height information and the offset information. The lamp group device 1 is compensated and adjusted according to the compensation data.
[0053] If the actual area is smaller than the effective area, it is judged that one or more of the actual lighting data, actual height data and actual offset data are smaller than the lighting information, height information and offset information input by the area algorithm when calculating the effective area. At this time, the compensation data includes the difference between the actual lighting data, actual height data and actual offset data and the lighting information, height information and offset information. The lamp group device 1 compensates and adjusts according to the compensation data.
[0054] The flight control system also includes a compensation judgment module, in which a judgment strategy is configured. The judgment strategy is specifically:
[0055] When the effective area is different from the actual area, the cause of the error is determined and failure data and / or physical damage data are generated, wherein the failure data indicates that the lighting lamp 4 has experienced use failure, and the physical damage indicates that the lamp assembly device 1 has experienced physical damage;
[0056] The flight control system generates maintenance data based on the exhaustion data and / or the physical damage data, and the maintenance data represents the area where the fault occurs and needs to be repaired.
[0057] As the lighting lamp 4 is used, it will generate heat and cause thermal damage to the lighting lamp 4. When the lighting lamp 4 is thermally damaged, the lighting brightness will decrease with the increase of the degree of thermal damage under the same input power. In response to this, the thermal damage will cause the lighting lamp 4 to fail, so that the effective area is different from the actual area. At this time, the flight control system will compensate. There are two compensation methods. One is to increase the input power of the failed lighting lamp 4 so that the lighting reaches the preset lighting level of the lighting information. The second is to turn off the failed lighting lamp 4 and control other lighting lamps 4 to compensate for the light to reach the effective area. When physical damage occurs, the effective area will also be different from the actual area. At this time, the lighting lamp 4 needs to be adjusted or repaired. The maintenance data is used to provide maintenance personnel with accurate positioning of the faulty area, so as to facilitate maintenance personnel to repair the faulty part to ensure that a light spot of an effective area can be formed.
[0058] Working principle and effect:
[0059] The spot matching strategy configured in the processor of the flight control system can calculate the effective area under the corresponding lighting information, height information and offset information, and compare the actual area with the effective area according to the spot recognition module and the spot compensation module. The light group device 1 is adjusted by the compensation data generated by the compensation strategy to match the actual area with the effective area, thereby forming sufficient lighting, providing a completely bright illumination spot, and improving the lighting efficiency.
[0060] The above is only a preferred embodiment of the present invention, and the protection scope of the present invention is not limited to the above embodiments. All technical solutions under the concept of the present invention belong to the protection scope of the present invention. It should be pointed out that for ordinary technicians in this technical field, some improvements and modifications without departing from the principle of the present invention should also be regarded as the protection scope of the present invention.
Claims
1. A lighting system for a tethered hovering platform, characterized in that: include: A light assembly device (1), the light assembly device (1) being arranged on a mooring platform, the light assembly device (1) comprising an adjusting mechanism (2) and a lighting mechanism (3), the lighting mechanism (3) comprising a plurality of lighting lamps (4) for providing lighting, the lighting mechanism (3) being connected to the adjusting mechanism (2), and the adjusting mechanism (2) being used to adjust the illumination angle of the lighting mechanism (3); A flight control system, the flight control system comprising a processor, a light spot control module, a height control module and an angle control module, the light spot control module being configured with preset lighting information, the light spot control module being used to control the lighting of an illumination lamp (4) providing illumination according to the lighting information, the lighting information representing the illumination angle of the illumination lamp (4), the height control module being configured with preset height information, the height control module being used to control and adjust the flight height of a tethered platform according to the height information, the height information representing the height of the tethered platform from an illumination surface, the angle control module being configured with preset offset information, the angle control module being used to adjust the angle of an illumination mechanism (3) according to the offset information, the offset information representing the offset inclination value of the illumination mechanism (3), the processor being configured with a light spot matching strategy and an area algorithm, the light spot matching strategy comprising retrieving the lighting information, the height information and the offset information and calculating the effective area of the illumination light spot according to the area algorithm, the processor being further configured with a memory unit, the memory unit being used to store the lighting information, the height information and the offset information corresponding to the effective area; The flight control system further comprises a light spot compensation module and a light spot recognition module. The light spot recognition module is used to obtain the actual light spot area formed and generate the actual area. The light spot recognition module also obtains the actual height of the moored platform to generate actual height data, and is also used to obtain the number and angle of the illuminated lighting lamps (4) to generate actual lighting data, and obtain the actual offset data of the lighting mechanism (3). The light spot compensation module is configured with a compensation strategy, which comprises calling the effective area and the actual area, and generating compensation data based on the comparison between the effective area and the actual area. The light group device (1) adjusts the irradiation mechanism and the adjustment mechanism (2) based on the compensation data.
2. The lighting system for a tethered hovering platform according to claim 1, characterized in that: The lighting mechanism (3) further comprises a lamp rack (31) and a lamp panel (32); the lamp rack (31) is connected to the mooring platform; a connecting shaft (33) is provided on the lamp rack (31); the lamp panel (32) is rotatably connected to the connecting shaft (33); a plurality of lamp slots are provided on the lamp panel (32); a lighting lamp (4) is installed in any of the lamp slots.
3. The lighting system for a tethered hovering platform according to claim 2, characterized in that: The regulating mechanism (2) comprises an regulating steering gear (21), an regulating gear (22) and a driven gear (23); the regulating steering gear (21) is connected to a lamp frame (31); the regulating gear (22) is coaxially fixedly connected to the regulating steering gear (21); and the driven gear (23) is connected to a lamp panel (32) and meshes with the regulating gear (22).
4. The lighting system for a tethered hovering platform according to claim 3, characterized in that: The light panels (32) are arranged in two symmetrical arrangements along a connecting shaft (33); an adjustment mechanism (2) is respectively arranged at one end of the two light panels (32) which are away from each other; and the two adjustment mechanisms (2) respectively control the tilting of the light panels (32) along the axis of the connecting shaft (33).
5. The lighting system for a tethered hovering platform according to claim 4, characterized in that: The area algorithm includes: s=π[(tanx° / 2)*h] 2 Among them: s represents the effective area, x represents the lighting information, and h represents the height information.
6. The lighting system for a tethered hovering platform according to claim 5, characterized in that: The area algorithm also includes: s=π{[tan(x°+y°) / 2]*h}[(tanx° / 2)*h] Among them: s represents the effective area, and y represents the offset information.
7. The lighting system for a tethered hovering platform according to claim 6, characterized in that: The area algorithm also includes: s=2π{[tan(x°+y°) / 2]*h}[tanx° / 2*h]*z Among them: z represents the combination coefficient.
8. The lighting system for a tethered hovering platform according to claim 7, characterized in that: The area algorithm also includes: s=π{[tan(x°+y°) / 2]*h}[(tanx° / 2)*h]*a*z Among them: a represents the number of lights on.
9. The lighting system for a tethered hovering platform according to claim 8, characterized in that: The compensation strategies include: If the actual area is larger than the effective area, it is determined that one or more of the actual lighting data, the actual height data and the actual offset data exceeds the input lighting information, height information and offset information of the area algorithm when calculating the effective area. At this time, the compensation data includes the difference between the actual lighting data, the actual height data and the actual offset data and the lighting information, the height information and the offset information. The lamp group device (1) is compensated and adjusted according to the compensation data. If the actual area is smaller than the effective area, it is determined that one or more of the actual lighting data, actual height data and actual offset data is smaller than the lighting information, height information and offset information input by the area algorithm when calculating the effective area. At this time, the compensation data includes the difference between the actual lighting data, actual height data and actual offset data and the lighting information, height information and offset information. The lamp group device (1) is compensated and adjusted according to the compensation data.
10. The lighting system for a tethered hovering platform according to any one of claims 1 to 9, characterized in that: The flight control system further includes a compensation judgment module, wherein a judgment strategy is configured in the compensation judgment module, and the judgment strategy is specifically: When the effective area is different from the actual area, determining the cause of the error and generating failure data and / or physical damage data, wherein the failure data indicates that the lighting lamp (4) has experienced use failure, and the physical damage data indicates that the lighting device (1) has experienced physical damage; The flight control system generates maintenance data according to the exhaustion data and / or the physical damage data, wherein the maintenance data represents an area where a fault occurs and needs maintenance.
Citation Information
Patent Citations
Mooring following system and method
CN105629995A
Lighting method and device of aircraft and aircraft
CN113064452A