CN204791568U - Flight system is followed to vehicle - Google Patents
Flight system is followed to vehicle Download PDFInfo
- Publication number
- CN204791568U CN204791568U CN201520587412.XU CN201520587412U CN204791568U CN 204791568 U CN204791568 U CN 204791568U CN 201520587412 U CN201520587412 U CN 201520587412U CN 204791568 U CN204791568 U CN 204791568U
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- vehicle
- aircraft
- control module
- flight system
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Abstract
The utility model relates to an aircraft technical field, in particular to flight system is followed to vehicle, including ranging module, control module, ranging module be used for measuring the positional information between aircraft and the vehicle and export positional information to control module, export the flight gesture of control command to aircraft adjustment aircraft to positional information after control module handles, the aircraft on still be provided with the camera unit who is used for detecting the ultrasonic sensor of aircraft the place ahead barrier and is used for acquireing the vehicle situation of traveling. Through ranging module and control module, guarantee that the aircraft flies in the vehicle certain limit, simultaneously, ultrasonic sensor avoids the aircraft to bump with the place ahead barrier when flight, acquires the situation of traveling of vehicle at last through camera unit, provides safeguard for the safety traffic of vehicle.
Description
Technical field
The utility model relates to vehicle technology field, and particularly flight system followed by a kind of vehicle.
Background technology
The model plane system of prior art is primarily of aircraft and telepilot composition, aircraft is equipped with radio system, telepilot is equipped with radio transmitting apparatus, its working method is: operator, by the environment around visual inspection model plane, uses a teleswitch and transmits control signal to control the motion of aircraft by the direct-connected mode of electromagnetic wave to model plane.The weak point of the method is: need people to carry out remote controller to reach the control of aircraft, and aircraft independently can not identify that automobile flight is followed to reach in path.
Utility model content
The purpose of this utility model is to provide a kind of vehicle to follow flight system, provides the visual field, high-altitude of vehicle to ensure the security that vehicle travels.
For realizing above object, the technical solution adopted in the utility model is: flight system followed by a kind of vehicle, comprise range finder module, control module, described range finder module is for the positional information measured between aircraft and vehicle and export positional information to control module, and control module location information carries out processing the flight attitude of rear output control command to aircraft adjustment aircraft; Described aircraft is also provided with for the ultrasonic sensor of sense aircraft preceding object thing and the image unit for obtaining traveling state of vehicle.
Compared with prior art, there is following technique effect in the utility model: by range finder module and control module, ensure that aircraft flies in vehicle certain limit, simultaneously, ultrasonic sensor avoids aircraft when flying and preceding object thing collides, the travel conditions of vehicle is obtained, for the safety traffic of vehicle provides safeguard finally by image unit.
Accompanying drawing explanation
Fig. 1 is theory diagram of the present utility model;
Fig. 2 is the structural representation that vehicle followed by the utility model aircraft.
Embodiment
Below in conjunction with Fig. 1 to Fig. 2, the utility model is described in further detail.
Consult Fig. 1, flight system followed by a kind of vehicle, comprise range finder module, control module, described range finder module is for the positional information measured between aircraft and vehicle and export positional information to control module, and control module location information carries out processing the flight attitude of rear output control command to aircraft adjustment aircraft; Described aircraft is also provided with for the ultrasonic sensor of sense aircraft preceding object thing and the image unit for obtaining traveling state of vehicle.Here the positional information between aircraft and vehicle is obtained by range finder module, then control module processes this positional information, here process can be carried out according to the actual needs, such as limit the height of aircraft within the scope of certain, once the height of aircraft is super go beyond the scope outside, just send corresponding control command to aircraft and adjust its height; Or the air line distance between restriction aircraft and vehicle is within the scope of certain, once the hypertelorism between aircraft and vehicle, then according to the azimuth information between aircraft and vehicle, the heading of aircraft, speed are adjusted, ensure that aircraft can follow vehicle reliably.Simultaneously, consider that aircraft is when following flight, vehicle up direction may occur that traffic lights, overline bridge etc. affect the barrier of aircraft flight, therefore be also provided with the barrier of ultrasonic sensor to aircraft front here to detect, and export result of detection to control module, control module exports the flight attitude of control command to aircraft adjustment aircraft according to result of detection, avoids colliding with barrier.Follow the prerequisite of vehicle at aircraft under, the image unit that aircraft is installed can obtain the aerial visual field effectively, transport condition and the periphery road conditions of vehicle can be found out intuitively according to the video information of image unit collection, as Train-borne recorder or trailer-mounted radar etc., monitoring blind area can not be there is.
As preferred version of the present utility model, described range finder module comprises electromagnetic positioning instrument or GPS unit and ultrasonic sensor, electromagnetic positioning instrument is for obtaining distance S between aircraft and vehicle and direction, GPS unit is for obtaining the horizontal range L between aircraft and vehicle, and ultrasonic sensor is for obtaining the flying height H of aircraft.Consult Fig. 2, because distance S here, horizontal range L, flying height H can be obtained by Pythagorean theorem, as long as therefore there are any two in electromagnetic positioning instrument, GPS unit, ultrasonic sensor three here, but consider that aircraft needs to use ultrasonic sensor when monitoring preceding object thing, from cost-saving angle, include ultrasonic sensor here and include any one in electromagnetic positioning instrument and GPS unit.
Preferably, this system also comprises the display unit be arranged on vehicle, and the video information that described image unit collects exports on display unit and shows after control module process.Vehicle shows video information that image unit collects in real time, facilitates the road conditions of driver to vehicle periphery to get more information about, make driver can make action in advance to potential danger, improve the security of driving.
Further, comprise and be arranged on carry-on storage unit, the video information that described image unit collects stores in the memory unit after control module process.On board the aircraft storage unit being installed, ensureing the loss of the video information that vehicle can not cause when having an accident image unit to gather.When storing, without the need to storing all video informations, only need the video information retaining nearest a period of time, the video information of other times more of a specified duration can delete to save storage space.
Further, comprise and be arranged on carry-on radar Doppler, described radar Doppler is used for the travel speed of collection vehicle and exports control module to.By arranging radar Doppler, monitor the travel speed of vehicle, on the one hand as the basis for estimation of accident in the future, can carry out danger warning when Vehicle Speed is too fast to driver on the other hand, prompting driver reduces travel speed.
Preferably, comprise and be arranged on carry-on gsm communication unit, described gsm communication unit gives the alarm to driver when vehicle travels abnormal and reports to the police to relevant departments when vehicle has an accident and send field accident photo.After gsm communication unit is set, can report to the police timely, improve the security that vehicle travels.
Claims (6)
1. flight system followed by a vehicle, it is characterized in that: comprise range finder module, control module, described range finder module is for the positional information measured between aircraft and vehicle and export positional information to control module, and control module location information carries out processing the flight attitude of rear output control command to aircraft adjustment aircraft; Described aircraft is also provided with for the ultrasonic sensor of sense aircraft preceding object thing and the image unit for obtaining traveling state of vehicle.
2. flight system followed by vehicle as claimed in claim 1, it is characterized in that: described range finder module comprises electromagnetic positioning instrument or GPS unit and ultrasonic sensor, electromagnetic positioning instrument is for obtaining distance S between aircraft and vehicle and direction, GPS unit is for obtaining the horizontal range L between aircraft and vehicle, and ultrasonic sensor is for obtaining the flying height H of aircraft.
3. flight system followed by vehicle as claimed in claim 1, and it is characterized in that: comprise the display unit be arranged on vehicle, the video information that described image unit collects exports on display unit and shows after control module process.
4. flight system followed by vehicle as claimed in claim 1, and it is characterized in that: comprise and be arranged on carry-on storage unit, the video information that described image unit collects stores in the memory unit after control module process.
5. flight system followed by vehicle as claimed in claim 1, it is characterized in that: comprise and be arranged on carry-on radar Doppler, and described radar Doppler is used for the travel speed of collection vehicle and exports control module to.
6. flight system followed by vehicle as claimed in claim 1, it is characterized in that: comprise and be arranged on carry-on gsm communication unit, described gsm communication unit gives the alarm to driver when vehicle travels abnormal and reports to the police to relevant departments when vehicle has an accident and send field accident photo.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520587412.XU CN204791568U (en) | 2015-08-07 | 2015-08-07 | Flight system is followed to vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520587412.XU CN204791568U (en) | 2015-08-07 | 2015-08-07 | Flight system is followed to vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204791568U true CN204791568U (en) | 2015-11-18 |
Family
ID=54531571
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520587412.XU Expired - Fee Related CN204791568U (en) | 2015-08-07 | 2015-08-07 | Flight system is followed to vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204791568U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109155103A (en) * | 2016-03-29 | 2019-01-04 | 福特全球技术公司 | With the real time communication of mobile infrastructure |
| CN109177753A (en) * | 2018-10-19 | 2019-01-11 | 如皋福大工程技术研究院有限公司 | Automobile-used aircraft and the automobile for carrying aircraft |
| CN112802369A (en) * | 2021-04-06 | 2021-05-14 | 北京三快在线科技有限公司 | Method and device for acquiring flight route, computer equipment and readable storage medium |
| CN112804441A (en) * | 2019-11-14 | 2021-05-14 | 长城汽车股份有限公司 | Unmanned aerial vehicle control method and device |
-
2015
- 2015-08-07 CN CN201520587412.XU patent/CN204791568U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109155103A (en) * | 2016-03-29 | 2019-01-04 | 福特全球技术公司 | With the real time communication of mobile infrastructure |
| CN109177753A (en) * | 2018-10-19 | 2019-01-11 | 如皋福大工程技术研究院有限公司 | Automobile-used aircraft and the automobile for carrying aircraft |
| CN112804441A (en) * | 2019-11-14 | 2021-05-14 | 长城汽车股份有限公司 | Unmanned aerial vehicle control method and device |
| CN112804441B (en) * | 2019-11-14 | 2022-11-11 | 长城汽车股份有限公司 | Unmanned aerial vehicle control method and device |
| CN112802369A (en) * | 2021-04-06 | 2021-05-14 | 北京三快在线科技有限公司 | Method and device for acquiring flight route, computer equipment and readable storage medium |
| CN112802369B (en) * | 2021-04-06 | 2021-07-16 | 北京三快在线科技有限公司 | Method and device for acquiring flight route, computer equipment and readable storage medium |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151118 Termination date: 20200807 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |