CN118163933B - Wireless remote control type airship with flight adjusting function - Google Patents
Wireless remote control type airship with flight adjusting function Download PDFInfo
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- CN118163933B CN118163933B CN202410291751.7A CN202410291751A CN118163933B CN 118163933 B CN118163933 B CN 118163933B CN 202410291751 A CN202410291751 A CN 202410291751A CN 118163933 B CN118163933 B CN 118163933B
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- 230000001276 controlling effect Effects 0.000 claims description 33
- 229910052734 helium Inorganic materials 0.000 claims description 11
- 239000001307 helium Substances 0.000 claims description 11
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 11
- 230000006870 function Effects 0.000 claims description 7
- 238000004880 explosion Methods 0.000 claims description 4
- 238000000034 method Methods 0.000 claims description 4
- 230000009711 regulatory function Effects 0.000 claims 1
- 238000005265 energy consumption Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 230000002035 prolonged effect Effects 0.000 description 2
- 230000035484 reaction time Effects 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/24—Arrangement of propulsion plant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/24—Arrangement of propulsion plant
- B64B1/30—Arrangement of propellers
- B64B1/32—Arrangement of propellers surrounding hull
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
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Abstract
The invention belongs to the technical field of wireless remote control airship, and particularly relates to a wireless remote control airship with a flight adjusting function, which comprises an airship body, wherein arc-shaped bodies are fixed on the periphery of the left and right sides of the airship body, an aerial photographing camera is arranged at the bottom of the airship body, tail wings are fixed on the outer sides of the arc-shaped bodies on the right side, a motor II is fixedly arranged on the right side of the airship body, and the output end of the motor II is fixedly connected with spiral blades; the eight arc-shaped bodies comprise a motor I, a propeller and a sleeve; a controller is arranged on the left side of the bottom of the airship body and is connected with a second motor and a first motor through wires respectively; the middle of the arc-shaped body is provided with an inclined hole, and the first motor is fixedly arranged in the inclined hole, so that the device solves the problem that the current wireless remote control airship cannot intelligently and freely and quickly adjust the flight direction of the airship and ensures the flight safety of the airship.
Description
Technical Field
The invention belongs to the technical field of wireless remote control airship, and particularly relates to a wireless remote control airship with a flight adjusting function.
Background
The airship is an aircraft lighter than air, the biggest difference with the hot air balloon is that the airship is provided with a device for propelling and controlling the flight state, the airship consists of a huge streamline boat body, a tail surface with a stable control function and a propelling device, the flying direction of the airship on the market is not well controlled when the airship flies, the using effect is poor, and the airship can collide with obstacles to damage the airship when the airship flies, so that the phenomenon becomes a problem to be solved urgently by people in the field.
Disclosure of Invention
The invention aims to provide a wireless remote control type airship with a flight adjusting function, so as to solve the problems in the background art.
In order to solve the technical problems, the invention provides the following technical scheme: the wireless remote control type airship with the flight adjusting function comprises an airship body, wherein arc-shaped bodies are fixed on the periphery of the left side and the right side of the airship body, an aerial photographing image head is arranged at the bottom of the airship body, tail wings are fixed on the outer sides of the arc-shaped bodies on the right side, a motor II is fixedly arranged on the right side of the airship body, and a spiral blade is fixedly connected to the output end of the motor II; the eight arc-shaped bodies comprise a motor I, a propeller and a sleeve; a controller is arranged on the left side of the bottom of the airship body and is connected with a second motor and a first motor through wires respectively; the middle of the arc-shaped body is provided with an inclined hole, the first motor is fixedly arranged in the inclined hole, the sleeve is fixedly arranged in the inclined hole, and the propeller is fixedly connected with the output end of the first motor and is positioned in the sleeve; the intelligent control system is electrically connected with eight motors respectively and is used for controlling the operation of the eight motors, so that the distributed rotation of eight propellers on the left side and the right side is controlled respectively.
Preferably, the intelligent control system comprises a wind direction judging module, a wind speed identifying module, a release valve control module, a time calculating module, a volume changing module and an intelligent control module, wherein an air pressure module is arranged in the release valve; the wind direction judging module and the wind speed identifying module are electrically connected with the volume changing module, the volume changing module is electrically connected with the time calculating module, and the air release valve control module is electrically connected with the time calculating module; the wind direction judging module, the wind speed identifying module, the air release valve control module, the time calculating module and the volume changing module are electrically connected with the intelligent control module, and the intelligent control module is electrically connected with the first motor and the second motor respectively.
Preferably, the wind direction judging module is used for judging whether the wireless remote control airship flies downwind or upwind, the wind speed identifying module is used for identifying the wind speed, wherein the wind speed comprises the wind speed of downwind and the wind speed of upwind, the air release valve control module is used for controlling the opening and closing of the air release valve, the time calculating module is used for calculating the time from the opening to the closing of the control valve, and the volume changing module is used for identifying the helium volume discharged by the wireless remote control airship according to the time from the opening to the closing of the control valve, so that the volume of the wireless remote control airship is calculated; the intelligent control module is used for controlling the running power of the first motor and the second motor according to the wind direction, the wind speed, the volume of the wireless remote control type airship, the resistance born by the wireless remote control type airship, the position height change, the wind speed change and the resistance change of the wireless remote control type airship, and the air pressure module is used for controlling the air release valve to run according to the air pressure in the airship body so as to release air from the airship body and perform air release control on the airship body to fall when the airship breaks down.
Preferably, the operation steps of the intelligent control system include: s1, floating after helium is filled in the wireless remote control type airship, and simultaneously, controlling the system to operate; s2, judging whether the wireless remote control type airship flies downwind or upwind, identifying the wind speed, controlling the opening and closing of a release valve in the flying process, changing the flying height of the wireless remote control type airship, calculating the time from the opening to the closing of the control valve, and identifying the helium discharge amount of the wireless remote control type airship according to the time from the opening to the closing of the control valve, so as to calculate the volume and the air pressure of the wireless remote control type airship, controlling the airship to release air through the release valve to prevent explosion, and controlling the airship to release air and drop through the release valve; s3, controlling the running power of the first motor and the second motor according to the wind direction, the wind speed, the self volume of the wireless remote control type airship, the resistance born by the wireless remote control type airship, the position and height change, the wind speed change and the resistance change of the wireless remote control type airship; and S4, after the flying is finished, controlling the air release valve to be opened until the wireless remote control airship lands, and stopping the intelligent control system.
Preferably, in the steps S2 and S3: in downwind mode: the larger the wind speed is, the larger the force of the boosting wireless remote control airship is, and meanwhile, the resistance value generated by the friction between the self volume of the wireless remote control airship and the air is added, so that the running power of the first control motor and the running power of the second control motor are small; in upwind mode: the larger the wind speed is, the larger the resistance of the wireless remote control airship is, and meanwhile, the resistance value generated by the friction between the self volume of the wireless remote control airship and the air is added, so that the running power of the first control motor and the running power of the second control motor are large.
Preferably, in the steps S2 and S3: the air release valve is opened and closed, the flying height of the wireless remote control type airship is lowered, and the lowering height of the wireless remote control type airship is judged according to the time length from the opening to the closing of the air release valve; in downwind mode: according to the change of the descending height, the wind force of downwind is reduced, the force of the boosting wireless remote control airship is reduced, meanwhile, the volume of the wireless remote control airship is reduced due to the air release of the air release valve, the resistance value generated by the friction between the volume of the wireless remote control airship and the air is reduced, and the running power of the motor II and the motor I is further reduced relatively; in upwind mode: the wind power is reduced, and meanwhile, the resistance value generated by the friction between the self volume of the wireless remote control airship and the air is reduced, so that the running power of the motor II and the motor I is reduced.
Preferably, in the step S2 and the step S3: when the aerial camera operates, the front obstacle is identified, and when the obstacle is identified, the operation power of the first control motor is maximized.
Compared with the prior art, the invention has the following beneficial effects: the intelligent control system adopted by the invention can not only meet the flight power of the wireless remote control type airship, but also relatively reduce the flight energy consumption of the wireless remote control type airship, so that the flight time of the wireless remote control type airship is prolonged, the use effect of the wireless remote control type airship is greatly enhanced, the operation power of the first motor and the second motor is slowed down after the wireless remote control type airship descends, the energy consumption can be greatly reduced, the descending wireless remote control type airship can fly stably relatively, the collision with obstacles caused by the too fast flight speed is prevented, the enough reaction time is provided for operators, and the protection capability of the wireless remote control type airship is improved.
Drawings
The accompanying drawings are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate the invention and together with the embodiments of the invention, serve to explain the invention. In the drawings:
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is an exploded view of the arcuate body of the present invention;
FIG. 3 is a diagram of the intelligent control system module connection of the present invention;
in the figure: 1. an airship body; 2. an arc body; 21. a first motor; 22. a propeller; 23. a sleeve; 24. an inclined hole; 3. a tail wing; 4. a second motor; 5. spiral leaves; 6. aerial photographing image heads; 7. and a controller.
Detailed Description
The technical scheme of the present invention is further described in non-limiting detail below with reference to the preferred embodiments and the accompanying drawings. It will be apparent that the described embodiments are only some, but not all, embodiments of the invention. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Referring to fig. 1-3, the present invention provides the following technical solutions: the wireless remote control type airship with the flight adjusting function comprises an airship body 1, wherein arc bodies 2 are fixed on the periphery of the left side and the right side of the airship body 1, an aerial photographing image head 6 is arranged at the bottom of the airship body 1, tail fins 3 are fixed on the outer sides of the right side arc bodies 2, a motor II 4 is fixedly arranged on the right side of the airship body 1, and spiral blades 5 are fixedly connected to the output ends of the motor II 4;
the eight arc bodies 2 comprise a motor one 21, a propeller 22 and a sleeve 23;
the left side of the bottom of the airship body 1 is provided with a controller 7, and the controller 7 is respectively connected with a second motor 4 and a first motor 21 through wires;
The middle of the arc body 2 is provided with an inclined hole 24, the first motor 21 is fixedly arranged in the inclined hole 24, the sleeve 23 is fixedly arranged in the inclined hole 24, and the propeller 22 is fixedly connected with the output end of the first motor 21 and is positioned in the sleeve 23;
The intelligent control system is electrically connected with eight motors 21 respectively and is used for controlling the operation of the eight motors 21, so that the distributed rotation of eight propellers 22 on the left side and the right side is controlled respectively;
The airship body 1 is filled with helium, then floats and flies upwards, the battery is filled with electricity to enable the controller 7 to operate, the controller 7 is electrically driven to enable the motor II 4 to operate in a remote control driving mode, the motor II 4 drives the screw blade 5 to rotate, thereby driving the wireless remote control airship to start flying, meanwhile, the aerial photographing imaging head 6 operates, the aerial photographing work is started, the remote control driving controller 7 enables the motor I21 to operate in the flying process, the motor I21 drives the screw propeller 22 to rotate, air flow is sprayed out through the inclined hole 24, so that the flying direction of the wireless remote control airship can be adjusted, and the angle adjustment of the airship is convenient and quick in a wireless driving mode, through all setting up screw 22 in wireless remote control formula airship left and right sides, can make the flying angle of wireless remote control formula airship fly time can freely be adjusted, through the running power of intelligent control system control motor two 4 and motor one 21, on the one hand reduce the energy consumption and use, on the other hand can improve the flying efficiency of wireless remote control formula airship, meet wind-force change automatically regulated flying power, the intellectuality is strong, the air release valve is used for controlling the helium tolerance in the airship body 1, thereby control the airship and float from top to bottom, control eight motors one 21 respectively through intelligent control system, thereby control eight screw 22 and rotate respectively, adjust the flying angle of wireless remote control formula airship:
when the wireless remote control airship ascends, the four propellers 22 at the lower left and lower right are controlled to rotate, and jet air flows are generated at the lower left and lower right;
When the wireless remote control airship descends, the four propellers 22 on the left and the right are controlled to rotate, and jet air flows are generated on the left and the right;
when the wireless remote control airship flies to the left and the rear, the four propellers 22 at the left front and the right rear are controlled to rotate, and jet air flows are generated at the left front and the right rear;
when the wireless remote control airship flies to the left front, the four propellers 22 at the left rear and the right front are controlled to rotate, and jet air flows are generated at the left rear and the right front;
When the wireless remote control airship hovers, the motor II 4 drives the screw blade 5 to stop rotating, and simultaneously the four screw propellers 22 at the lower left and the upper left rotate to generate reverse thrust, so that the wireless remote control airship is stopped, and after the wireless remote control airship is stopped, the four screw propellers 22 at the lower left and the lower right are controlled to intermittently rotate, and air flow is intermittently sprayed, so that the wireless remote control airship hovers.
The intelligent control system comprises a wind direction judging module, a wind speed identifying module, a release valve control module, a time calculating module, a volume changing module and an intelligent control module, wherein an air pressure module is arranged in the release valve;
The wind direction judging module and the wind speed identifying module are electrically connected with the volume changing module, the volume changing module is electrically connected with the time calculating module, and the air release valve control module is electrically connected with the time calculating module;
the wind direction judging module, the wind speed identifying module, the air release valve control module, the time calculating module and the volume changing module are electrically connected with the intelligent control module, and the intelligent control module is electrically connected with the first motor 21 and the second motor 4 respectively.
The wind direction judging module is used for judging whether the wireless remote control type airship flies downwind or upwind, the wind speed identifying module is used for identifying the wind speed, wherein the wind speed comprises the wind speed of downwind and the wind speed of upwind, the air release valve control module is used for controlling the opening and closing of the air release valve, the time calculating module is used for calculating the time from the opening to the closing of the control valve, and the volume changing module is used for identifying the helium amount discharged by the wireless remote control type airship according to the time from the opening to the closing of the control valve, so that the volume of the wireless remote control type airship is calculated;
The intelligent control module is used for controlling the running power of the first motor 21 and the second motor 4 according to the wind direction, the wind speed, the volume of the wireless remote control type airship, the resistance born by the wireless remote control type airship, the position height change, the wind speed change and the resistance change of the wireless remote control type airship, and the air pressure module is used for controlling the air release valve to run according to the air pressure in the airship body 1, so that the airship body 1 is released, and the airship body 1 is controlled to fall when the airship breaks down.
The intelligent control system comprises the following operation steps:
s1, floating after helium is filled in the wireless remote control type airship, and simultaneously, controlling the system to operate;
S2, judging whether the wireless remote control type airship flies downwind or upwind, identifying the wind speed, controlling the air release valve to be opened and closed in the flying process, changing the flying height of the wireless remote control type airship, calculating the time from the opening to the closing of the control valve, and identifying the helium discharge amount of the wireless remote control type airship according to the time from the opening to the closing of the control valve, so as to calculate the volume of the wireless remote control type airship, controlling the airship to release air through the air release valve when the air pressure of the airship is large, preventing explosion, and controlling the airship to release air and fall through the air release valve when the air release valve fails;
S3, controlling the running power of the first motor 21 and the second motor 4 according to the wind direction, the wind speed, the self volume of the wireless remote control type airship, the resistance born by the wireless remote control type airship, the position and height change, the wind speed change and the resistance change of the wireless remote control type airship;
and S4, after the flying is finished, controlling the air release valve to be opened until the wireless remote control airship lands, and stopping the intelligent control system.
In steps S2 and S3:
In downwind mode: the larger the wind speed is, the larger the force of the boosting wireless remote control airship is, and meanwhile, the resistance value generated by the friction between the self volume of the wireless remote control airship and the air is added, so that the running power of the first motor 21 and the running power of the second motor 4 are controlled to be small;
in upwind mode: the larger the wind speed is, the larger the resistance of the wireless remote control airship is, and meanwhile, the resistance value generated by the friction between the self volume of the wireless remote control airship and the air is added, so that the running power of the first motor 21 and the running power of the second motor 4 are controlled to be large;
The flying power of the wireless remote control type airship can be met, and the flying energy consumption of the wireless remote control type airship can be relatively reduced, so that the flying time of the wireless remote control type airship is prolonged, and the using effect of the wireless remote control type airship is greatly enhanced.
In steps S2 and S3:
the air release valve is opened and closed, the flying height of the wireless remote control type airship is lowered, and the lowering height of the wireless remote control type airship is judged according to the time length from the opening to the closing of the air release valve;
In downwind mode: according to the change of the descending height, the wind force of downwind is reduced, the force of the boosting wireless remote control airship is reduced, meanwhile, the volume of the wireless remote control airship is reduced due to the air release of the air release valve, the resistance value generated by the friction between the volume of the wireless remote control airship and the air is reduced, and the running power of the motor II 4 and the motor I21 is further reduced relatively;
in upwind mode: the wind power is reduced, and meanwhile, the resistance value generated by the friction between the self volume of the wireless remote control airship and the air is reduced, so that the running power of the motor II 4 and the motor I21 is reduced;
After the wireless remote control type airship descends, the running power of the first motor 21 and the second motor 4 is slowed down, the energy consumption can be greatly reduced, meanwhile, the descending wireless remote control type airship can fly stably relatively, collision with obstacles caused by too high flying speed is prevented, enough reaction time can be given to operators, and the protection capability of the wireless remote control type airship is improved.
In step S2 and step S3:
identifying a front obstacle when the aerial photographing camera 6 operates, and controlling the operation power of the first motor 21 to be maximized when the obstacle is identified;
can make wireless remote control formula airship carry out emergency avoidance when just touching the barrier, further protect wireless remote control formula airship, and when the airship atmospheric pressure is great, let out air through air release valve control airship, prevent that the airship from causing the explosion because inside atmospheric pressure is too big, and when the airship breaks down, let out air through air release valve control airship and descend, play the effect of fully protecting the airship.
In the description of the present invention, it should be understood that the directions or positional relationships indicated by the terms "upper", "lower", "front", "rear", "left", "right", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present invention, and do not indicate or imply that the apparatus or elements referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention.
Finally, it should be pointed out that: the above embodiments are only for illustrating the technical solution of the present invention, and are not limiting. Although the invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may be modified or some technical features may be equivalently replaced, and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the embodiments of the present invention.
Claims (2)
1. The utility model provides a wireless remote control formula airship with flight regulatory function, includes airship body (1), its characterized in that: arc bodies (2) are fixed on the periphery of the left side and the right side of the airship body (1), an aerial camera (6) is arranged at the bottom of the airship body (1), tail wings (3) are fixed on the outer sides of the arc bodies (2) on the right side, a motor II (4) is fixedly arranged on the right side of the airship body (1), and spiral blades (5) are fixedly connected to the output end of the motor II (4);
The eight arc-shaped bodies (2) comprise a motor I (21), a propeller (22) and a sleeve (23);
a controller (7) is arranged on the left side of the bottom of the airship body (1), and the controller (7) is respectively connected with a second motor (4) and a first motor (21) through wires;
The middle of the arc-shaped body (2) is provided with an inclined hole (24), the first motor (21) is fixedly arranged in the inclined hole (24), the sleeve (23) is fixedly arranged in the inclined hole (24), and the propeller (22) is fixedly connected with the output end of the first motor (21) and is positioned in the sleeve (23);
An intelligent control system and a battery are arranged in the controller (7), an air release valve is connected between the interior and the exterior of the airship body (1), the intelligent control system is respectively and electrically connected with eight motors (21) and is used for controlling the operation of the eight motors (21) so as to respectively control the distributed rotation of eight propellers (22) on the left side and the right side, the intelligent control system comprises a wind direction judging module, a wind speed identifying module, an air release valve control module, a time calculating module, a volume changing module and an intelligent control module, and an air pressure module is arranged in the air release valve;
The wind direction judging module and the wind speed identifying module are electrically connected with the volume changing module, the volume changing module is electrically connected with the time calculating module, and the air release valve control module is electrically connected with the time calculating module;
The intelligent control system comprises a wind direction judging module, a wind speed identifying module, a release valve control module, a time calculating module and a volume changing module, wherein the wind direction judging module, the wind speed identifying module, the release valve control module, the time calculating module and the volume changing module are all electrically connected with the intelligent control module, the intelligent control module is respectively electrically connected with a first motor (21) and a second motor (4), the wind direction judging module is used for judging whether the wireless remote control airship flies downwind or upwind, the wind speed identifying module is used for identifying the wind speed and the wind speed of upwind, wherein the wind speed comprises the wind speed of downwind and the wind speed of upwind, the release valve control module is used for controlling the release valve to be opened and closed, the time calculating module is used for calculating the time between the opening and the closing of the control valve, and the volume changing module is used for identifying the helium discharge amount of the wireless remote control airship according to the time between the opening and the closing of the control valve, so that the volume of the wireless remote control airship is calculated;
The intelligent control module is used for controlling the running power of a motor I (21) and a motor II (4) according to the wind direction, the wind speed, the volume of the wireless remote control type airship, the resistance born by the wireless remote control type airship, the position height change, the wind speed change and the resistance change of the wireless remote control type airship, and the air pressure module is used for controlling the operation of an air release valve according to the air pressure inside the airship body (1), so as to release air to the airship body (1) and perform air release control on the airship body (1) to fall when the airship breaks down, and the intelligent control system comprises the following operation steps:
s1, floating after helium is filled in the wireless remote control type airship, and simultaneously, controlling the system to operate;
S2, judging whether the wireless remote control type airship flies downwind or upwind, identifying the wind speed, controlling the air release valve to be opened and closed in the flying process, changing the flying height of the wireless remote control type airship, calculating the time from the opening to the closing of the control valve, and identifying the helium discharge amount of the wireless remote control type airship according to the time from the opening to the closing of the control valve, so as to calculate the volume of the wireless remote control type airship, controlling the airship to release air through the air release valve when the air pressure of the airship is large, preventing explosion, and controlling the airship to release air and fall through the air release valve when the air release valve fails;
s3, controlling the running power of the motor I (21) and the motor II (4) according to the wind direction, the wind speed, the self volume of the wireless remote control type airship, the resistance born by the wireless remote control type airship, the position and height change, the wind speed change and the resistance change of the wireless remote control type airship;
and S4, after the flight is finished, controlling the air release valve to be opened until the wireless remote control airship lands, and stopping the intelligent control system, wherein in the steps S2 and S3:
In downwind mode: the larger the wind speed is, the larger the force of the boosting wireless remote control airship is, and meanwhile, the resistance value generated by the friction between the self volume of the wireless remote control airship and the air is added, so that the running power of the first control motor (21) and the second control motor (4) is small;
In upwind mode: the larger the wind speed is, the larger the resistance to the wireless remote control airship is, and meanwhile, the resistance value generated by the friction between the self volume of the wireless remote control airship and the air is added, so that the running power of the first motor (21) and the running power of the second motor (4) are controlled to be large, and in the steps S2 and S3:
the air release valve is opened and closed, the flying height of the wireless remote control type airship is lowered, and the lowering height of the wireless remote control type airship is judged according to the time length from the opening to the closing of the air release valve;
In downwind mode: according to the change of the descending height, the wind force of downwind is reduced, the force of the boosting wireless remote control airship is reduced, meanwhile, the volume of the wireless remote control airship is reduced due to the air release of an air release valve, the resistance value generated by the friction between the volume of the wireless remote control airship and the air is reduced, and the running power of a motor II (4) and a motor I (21) is further reduced relatively;
In upwind mode: the wind power is reduced, and meanwhile, the resistance value generated by the friction between the self volume of the wireless remote control airship and the air is reduced, so that the running power of the motor II (4) and the motor I (21) is reduced.
2. A wireless remote control airship with flight adjustment function according to claim 1, characterized in that: in the steps S2 and S3:
the front obstacle is identified when the aerial camera (6) operates, and when the obstacle is identified, the operation power of the first control motor (21) is maximized.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202410291751.7A CN118163933B (en) | 2024-03-14 | 2024-03-14 | Wireless remote control type airship with flight adjusting function |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202410291751.7A CN118163933B (en) | 2024-03-14 | 2024-03-14 | Wireless remote control type airship with flight adjusting function |
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| CN118163933A CN118163933A (en) | 2024-06-11 |
| CN118163933B true CN118163933B (en) | 2024-09-13 |
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Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101885378A (en) * | 2010-07-06 | 2010-11-17 | 张朝林 | Inflation airship |
| CN103303457A (en) * | 2013-06-06 | 2013-09-18 | 北京新誉防务技术研究院有限公司 | Soft and hard hybrid airship and control method thereof |
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