CN202499280U - Unmanned device self stabilization holder - Google Patents
Unmanned device self stabilization holder Download PDFInfo
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- CN202499280U CN202499280U CN2011205644172U CN201120564417U CN202499280U CN 202499280 U CN202499280 U CN 202499280U CN 2011205644172 U CN2011205644172 U CN 2011205644172U CN 201120564417 U CN201120564417 U CN 201120564417U CN 202499280 U CN202499280 U CN 202499280U
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- setting device
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- angle degree
- degree setting
- servo drive
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Abstract
The utility model provides an unmanned device self stabilization holder capable of performing X/Y/Z triaxial control and automatically horizontal stabilizing, which comprises an airborne attitude sensor, a one-chip microcomputer connected to the airborne attitude sensor, a servo drive unit connected with the one-chip microcomputer, a X axis angular adjustment apparatus, a Y axis angular adjustment apparatus and a Z axis angular adjustment apparatus driven by the servo drive unit; the one-chip microcomputer is used for receiving the data of the airborne attitude sensor, and the data is calculated to obtain the servo driving information, the servo driving information is sent to the servo drive unit, and the corresponding X axis angular adjustment apparatus, the Y axis angular adjustment apparatus and the Z axis angular adjustment apparatus can be driven by the servo drive unit. The unmanned device self stabilization holder is characterized in that the ground staff can control the apparatus such as high definition digital camera to perform X axis motion, Y axis motion and Z axis motion through ground, thereby the image stability and the orientation accuracy can be reached.
Description
Technical field
The utility model relates to a kind of unmanned plane assembly, especially a kind of unmanned plane self-stabilization The Cloud Terrace.
Background technology
Unmanned plane self-stabilization The Cloud Terrace is the installation and control platform of unmanned aerial vehicle onboard sensor, and unmanned plane is in flight course, and self orientation can change, and the orientation of the airborne sensor that is also changes thereupon, can't guarantee the normal operation of sensor.
The utility model content
The purpose of the utility model provides a kind of X/Y/Z of carrying out three axle controls and the stable unmanned plane self-stabilization The Cloud Terrace of automatic horizontal.
Realize the unmanned plane self-stabilization The Cloud Terrace of the utility model purpose; Comprise airborne attitude sensor; The micro controller system that links to each other with said airborne attitude sensor; The servo drive that links to each other with said micro controller system is by X shaft angle degree setting device, Y shaft angle degree setting device and the Z shaft angle degree setting device of said servo drive driving;
Said micro controller system is used to receive the data of airborne attitude sensor; These data of union obtain servo driving information; And this servo driving information passed to servo drive, drive corresponding X shaft angle degree setting device, Y shaft angle degree setting device and Z shaft angle degree setting device by servo drive.
The rotatable 120 degree angles of said X shaft angle degree setting device.
The rotatable 120 degree angles of said Y shaft angle degree setting device.
The rotatable 360 degree angles of said Z shaft angle degree setting device.
The beneficial effect of the unmanned plane self-stabilization The Cloud Terrace of the utility model is following:
The unmanned plane self-stabilization The Cloud Terrace of the utility model; Make the ground staff can be right, carry out the 120 degree motions of X axle, Y axle 120 degree like high definition digital camera etc. through ground control equipment; The 360 degree motions of Z axle; And can carry out the stable correction of automatic level, vertical direction to three of X/Y/Z carrying under the motion of machine mal, make it reach the accuracy in the degree of stability and the orientation of image.
Description of drawings
Fig. 1 is the structural representation of the unmanned plane self-stabilization The Cloud Terrace of the utility model.
The specific embodiment
The embodiment of the utility model is following:
As shown in Figure 1; The unmanned plane self-stabilization The Cloud Terrace of the utility model; Comprise the micro controller system that airborne attitude sensor links to each other with said airborne attitude sensor; The servo drive that links to each other with said micro controller system is by X shaft angle degree setting device, Y shaft angle degree setting device and the Z shaft angle degree setting device of said servo drive driving;
Said micro controller system is used to receive the data of airborne attitude sensor; These data of union obtain servo driving information; And this servo driving information passed to servo drive, drive corresponding X shaft angle degree setting device, Y shaft angle degree setting device and Z shaft angle degree setting device by servo drive.
The rotatable 120 degree angles of said X shaft angle degree setting device.The rotatable 120 degree angles of said Y shaft angle degree setting device.The rotatable 360 degree angles of said Z shaft angle degree setting device.
The advantage of the unmanned plane self-stabilization The Cloud Terrace of the utility model is following:
1, axial each the servomotor d-axis of X/Y/Z does not have the return difference influence of retarder, high precision, high rigidity.
2, use current sensor to make up electric current loop and use photoelectric encoder to make up ring in the speed, give full play to the potentiality of torque motor.
3, select the single shaft spiral appearance of low drift ST series for use, additional precision accelerometer provides and returns flat function faster.
Embodiment recited above describes the preferred implementation of the utility model; Be not that scope to the utility model limits; Design under the spiritual prerequisite not breaking away from the utility model; Various distortion and improvement that the common engineering staff in this area make the utility model technical scheme all should fall in the protection domain that claims of the utility model confirm.
Claims (4)
1. unmanned plane self-stabilization The Cloud Terrace; It is characterized in that: comprise airborne attitude sensor; The micro controller system that links to each other with said airborne attitude sensor; The servo drive that links to each other with said micro controller system is by X shaft angle degree setting device, Y shaft angle degree setting device and the Z shaft angle degree setting device of said servo drive driving;
Said micro controller system is used to receive the data of airborne attitude sensor; These data of union obtain servo driving information; And this servo driving information passed to servo drive, drive corresponding X shaft angle degree setting device, Y shaft angle degree setting device and Z shaft angle degree setting device by servo drive.
2. unmanned plane self-stabilization The Cloud Terrace according to claim 1 is characterized in that: the rotatable 120 degree angles of said X shaft angle degree setting device.
3. unmanned plane self-stabilization The Cloud Terrace according to claim 1 is characterized in that: the rotatable 120 degree angles of said Y shaft angle degree setting device.
4. unmanned plane self-stabilization The Cloud Terrace according to claim 1 is characterized in that: the rotatable 360 degree angles of said Z shaft angle degree setting device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205644172U CN202499280U (en) | 2011-12-29 | 2011-12-29 | Unmanned device self stabilization holder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205644172U CN202499280U (en) | 2011-12-29 | 2011-12-29 | Unmanned device self stabilization holder |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202499280U true CN202499280U (en) | 2012-10-24 |
Family
ID=47035903
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205644172U Expired - Fee Related CN202499280U (en) | 2011-12-29 | 2011-12-29 | Unmanned device self stabilization holder |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202499280U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103775840A (en) * | 2014-01-01 | 2014-05-07 | 许洪 | Emergency lighting system |
| CN105607653A (en) * | 2016-01-05 | 2016-05-25 | 深圳一电航空技术有限公司 | Holder control method and system |
| WO2017143595A1 (en) * | 2016-02-26 | 2017-08-31 | Sz Dji Osmo Technology Co., Ltd. | Method and system for stabilizing a payload |
| WO2019051640A1 (en) * | 2017-09-12 | 2019-03-21 | 深圳市大疆灵眸科技有限公司 | Control method for pan-tilt, controller, and pan-tilt |
| CN109835495A (en) * | 2017-11-29 | 2019-06-04 | 云南电网有限责任公司玉溪供电局 | A kind of aircraft inclination flight Self-stabilization holder |
| US11225260B2 (en) | 2017-03-28 | 2022-01-18 | Beijing Jingdong Qianshi Technology Co., Ltd. | Control method and device for automated guided vehicle, and automated guided vehicle |
-
2011
- 2011-12-29 CN CN2011205644172U patent/CN202499280U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103775840A (en) * | 2014-01-01 | 2014-05-07 | 许洪 | Emergency lighting system |
| CN105607653A (en) * | 2016-01-05 | 2016-05-25 | 深圳一电航空技术有限公司 | Holder control method and system |
| WO2017143595A1 (en) * | 2016-02-26 | 2017-08-31 | Sz Dji Osmo Technology Co., Ltd. | Method and system for stabilizing a payload |
| CN107922056A (en) * | 2016-02-26 | 2018-04-17 | 深圳市大疆灵眸科技有限公司 | Method and system for steady load |
| US10330254B2 (en) | 2016-02-26 | 2019-06-25 | Sz Dji Osmo Technology Co., Ltd. | Method and system for stabilizing a payload |
| CN107922056B (en) * | 2016-02-26 | 2021-03-23 | 深圳市大疆灵眸科技有限公司 | Method and system for stabilizing a load |
| US11118728B2 (en) | 2016-02-26 | 2021-09-14 | Sz Dji Osmo Technology Co., Ltd. | Method and system for stabilizing a payload |
| US11225260B2 (en) | 2017-03-28 | 2022-01-18 | Beijing Jingdong Qianshi Technology Co., Ltd. | Control method and device for automated guided vehicle, and automated guided vehicle |
| WO2019051640A1 (en) * | 2017-09-12 | 2019-03-21 | 深圳市大疆灵眸科技有限公司 | Control method for pan-tilt, controller, and pan-tilt |
| US11156905B2 (en) | 2017-09-12 | 2021-10-26 | Sz Dji Osmo Technology Co., Ltd. | Control method for gimbal, controller, and gimbal |
| CN109835495A (en) * | 2017-11-29 | 2019-06-04 | 云南电网有限责任公司玉溪供电局 | A kind of aircraft inclination flight Self-stabilization holder |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| DD01 | Delivery of document by public notice |
Addressee: China Ewatt Technology Co., Ltd. Document name: Notification to Pay the Fees |
|
| DD01 | Delivery of document by public notice |
Addressee: China Ewatt Technology Co., Ltd. Document name: Notification of Termination of Patent Right |
|
| DD01 | Delivery of document by public notice |
Addressee: China Ewatt Technology Co., Ltd. Document name: Notification of Decision on Request for Restoration of Right |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121024 Termination date: 20181229 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |