CN113853560A - 飞行控制方法和设备 - Google Patents
飞行控制方法和设备 Download PDFInfo
- Publication number
- CN113853560A CN113853560A CN202080033691.9A CN202080033691A CN113853560A CN 113853560 A CN113853560 A CN 113853560A CN 202080033691 A CN202080033691 A CN 202080033691A CN 113853560 A CN113853560 A CN 113853560A
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- unmanned aerial
- aerial vehicle
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- control mode
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- 238000000034 method Methods 0.000 title claims abstract description 61
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title claims abstract description 49
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Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
一种无人机的飞行控制方法和设备,获取无人机的飞行高度(S301),确定飞行高度是否满足第一预设高度条件(S302),若是,控制无人机由第一控制模式切换至第二控制模式(S303),其中,响应于遥控器的同一运动控制指令,无人机在第一控制模式下的第一运动变化量大于在第二控制模式下的第二运动变化量,更容易调整飞行姿态,减少出现飞机炸机次数。
Description
PCT国内申请,说明书已公开。
Claims (32)
- PCT国内申请,权利要求书已公开。
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/CN2020/092555 WO2021237500A1 (zh) | 2020-05-27 | 2020-05-27 | 飞行控制方法和设备 |
Publications (1)
Publication Number | Publication Date |
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CN113853560A true CN113853560A (zh) | 2021-12-28 |
Family
ID=78745197
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202080033691.9A Pending CN113853560A (zh) | 2020-05-27 | 2020-05-27 | 飞行控制方法和设备 |
Country Status (2)
Country | Link |
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CN (1) | CN113853560A (zh) |
WO (1) | WO2021237500A1 (zh) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114237051B (zh) * | 2021-12-16 | 2023-05-23 | 江苏理工学院 | 基于分数阶滑模反步法的动力翼伞高度控制方法 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103383571B (zh) * | 2013-08-13 | 2016-03-30 | 湖南航天机电设备与特种材料研究所 | 一种非对称四旋翼无人机及其控制方法 |
US9745013B2 (en) * | 2015-10-15 | 2017-08-29 | Focus Designs Inc. | Self-balancing electric vehicle with strain-based controls |
CN105404305B (zh) * | 2015-12-29 | 2018-12-18 | 小米科技有限责任公司 | 平衡车的控制方法和控制装置 |
CN107390708A (zh) * | 2017-08-22 | 2017-11-24 | 成都飞机工业(集团)有限责任公司 | 一种基于鲁棒伺服控制无人机起飞拉起的方法 |
US10856542B2 (en) * | 2017-11-30 | 2020-12-08 | Florida Power & Light Company | Unmanned aerial vehicle system for deterring avian species from sensitive areas |
CN108267961A (zh) * | 2018-02-11 | 2018-07-10 | 浙江工业大学 | 基于对称时变正切型约束李雅普诺夫函数的四旋翼飞行器全状态受限控制方法 |
US10909864B2 (en) * | 2018-06-27 | 2021-02-02 | Intel Corporation | Drone obstacle avoidance using real-time wind estimation |
CN110531779A (zh) * | 2019-08-02 | 2019-12-03 | 杭州电子科技大学 | 一种无人机仿人协同飞行控制器及其实现方法 |
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2020
- 2020-05-27 CN CN202080033691.9A patent/CN113853560A/zh active Pending
- 2020-05-27 WO PCT/CN2020/092555 patent/WO2021237500A1/zh active Application Filing
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WO2021237500A1 (zh) | 2021-12-02 |
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