CN108549400B - 基于对数增强型双幂次趋近律和快速终端滑模面的四旋翼飞行器自适应控制方法 - Google Patents
基于对数增强型双幂次趋近律和快速终端滑模面的四旋翼飞行器自适应控制方法 Download PDFInfo
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- CN108549400B CN108549400B CN201810519661.3A CN201810519661A CN108549400B CN 108549400 B CN108549400 B CN 108549400B CN 201810519661 A CN201810519661 A CN 201810519661A CN 108549400 B CN108549400 B CN 108549400B
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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
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
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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
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Feedback Control In General (AREA)
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CN201810519661.3A CN108549400B (zh) | 2018-05-28 | 2018-05-28 | 基于对数增强型双幂次趋近律和快速终端滑模面的四旋翼飞行器自适应控制方法 |
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CN201810519661.3A CN108549400B (zh) | 2018-05-28 | 2018-05-28 | 基于对数增强型双幂次趋近律和快速终端滑模面的四旋翼飞行器自适应控制方法 |
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CN108549400A CN108549400A (zh) | 2018-09-18 |
CN108549400B true CN108549400B (zh) | 2021-08-03 |
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AU2018456069A1 (en) * | 2018-12-31 | 2021-08-12 | Kimberly-Clark Worldwide, Inc. | Absorbent articles with curved elasticized laminates |
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US6684147B2 (en) * | 2001-12-17 | 2004-01-27 | Hydro-Aire, Inc. | Sliding integral proportional (SIP) controller for aircraft skid control |
US7453227B2 (en) * | 2005-12-20 | 2008-11-18 | Intuitive Surgical, Inc. | Medical robotic system with sliding mode control |
EA024007B1 (ru) * | 2007-08-09 | 2016-08-31 | ЭлТиЭй КОРПОРЕЙШН | Системы и способ для отображения информации положения в пространстве, связанной с дирижаблем |
US8006070B2 (en) * | 2007-12-05 | 2011-08-23 | International Business Machines Corporation | Method and apparatus for inhibiting fetch throttling when a processor encounters a low confidence branch instruction in an information handling system |
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CN107368089B (zh) * | 2017-07-11 | 2019-12-03 | 浙江工业大学 | 一种基于双指数型函数的四旋翼飞行器非线性滑模位姿控制方法 |
CN107368088B (zh) * | 2017-07-11 | 2019-12-03 | 浙江工业大学 | 一种基于误差指数型函数的四旋翼飞行器非线性滑模位姿控制方法 |
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KR101667015B1 (ko) * | 2015-03-17 | 2016-10-17 | 신형호 | 한 손 조작이 가능한 멀티로터 컨트롤러 |
CN107688295A (zh) * | 2017-08-29 | 2018-02-13 | 浙江工业大学 | 一种基于快速终端滑模的四旋翼飞行器有限时间自适应控制方法 |
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Application publication date: 20180918 Assignee: Zhejiang puyun Technology Co.,Ltd. Assignor: JIANG University OF TECHNOLOGY Contract record no.: X2023980037552 Denomination of invention: Adaptive Control Method for Quadcopter Aircraft Based on Logarithmic Enhanced Double Power Reaching Law and Fast Terminal Sliding Mode Surface Granted publication date: 20210803 License type: Common License Record date: 20230706 |
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Application publication date: 20180918 Assignee: Foshan chopsticks Technology Co.,Ltd. Assignor: JIANG University OF TECHNOLOGY Contract record no.: X2024980000084 Denomination of invention: Adaptive Control Method for Quadcopter Aircraft Based on Logarithmic Enhanced Double Power Reaching Law and Fast Terminal Sliding Mode Surface Granted publication date: 20210803 License type: Common License Record date: 20240104 |