CN108241293B - 一种基于推演导数的过失速机动迎角控制方法 - Google Patents
一种基于推演导数的过失速机动迎角控制方法 Download PDFInfo
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- CN108241293B CN108241293B CN201711293811.5A CN201711293811A CN108241293B CN 108241293 B CN108241293 B CN 108241293B CN 201711293811 A CN201711293811 A CN 201711293811A CN 108241293 B CN108241293 B CN 108241293B
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
- G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
- G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
- G05B13/042—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators in which a parameter or coefficient is automatically adjusted to optimise the performance
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- Software Systems (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Feedback Control In General (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
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CN201711293811.5A CN108241293B (zh) | 2017-12-08 | 2017-12-08 | 一种基于推演导数的过失速机动迎角控制方法 |
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CN201711293811.5A CN108241293B (zh) | 2017-12-08 | 2017-12-08 | 一种基于推演导数的过失速机动迎角控制方法 |
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CN108241293A CN108241293A (zh) | 2018-07-03 |
CN108241293B true CN108241293B (zh) | 2020-02-14 |
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6188330B1 (en) * | 1999-02-01 | 2001-02-13 | Alliedsignal, Inc. | Windshear detection system |
CN102360216A (zh) * | 2011-05-20 | 2012-02-22 | 南京航空航天大学 | 双发舰载飞机单发停车的安全着舰控制方法 |
CN105138012A (zh) * | 2015-09-09 | 2015-12-09 | 南京航空航天大学 | 一种gps引导的无人机自动着舰自适应控制***及方法 |
CN105843080A (zh) * | 2016-06-01 | 2016-08-10 | 南京航空航天大学 | 可变翼高超声速飞行器智能非线性控制*** |
CN106864731A (zh) * | 2015-12-11 | 2017-06-20 | 中国航空工业集团公司成都飞机设计研究所 | 一种飞机大迎角俯仰控制方法 |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7043345B2 (en) * | 2003-10-10 | 2006-05-09 | Raytheon Company | System and method with adaptive angle-of-attack autopilot |
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2017
- 2017-12-08 CN CN201711293811.5A patent/CN108241293B/zh active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6188330B1 (en) * | 1999-02-01 | 2001-02-13 | Alliedsignal, Inc. | Windshear detection system |
CN102360216A (zh) * | 2011-05-20 | 2012-02-22 | 南京航空航天大学 | 双发舰载飞机单发停车的安全着舰控制方法 |
CN105138012A (zh) * | 2015-09-09 | 2015-12-09 | 南京航空航天大学 | 一种gps引导的无人机自动着舰自适应控制***及方法 |
CN106864731A (zh) * | 2015-12-11 | 2017-06-20 | 中国航空工业集团公司成都飞机设计研究所 | 一种飞机大迎角俯仰控制方法 |
CN105843080A (zh) * | 2016-06-01 | 2016-08-10 | 南京航空航天大学 | 可变翼高超声速飞行器智能非线性控制*** |
Non-Patent Citations (4)
Title |
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一种改进的非定常气动力模糊逻辑建模方法;吕永玺等;《西北工业大学学报》;20151231;第33卷(第6期);第971-976页 * |
先进飞行器非定常气动力建模、控制律设计及验证方法研究;龚正;《工程科技II辑》;20120715;第C031-7页 * |
基于被控变量设计的飞机动态逆控制律;李导等;《四川大学学报(自然科学版)》;20140131;第51卷(第1期);第95-100页 * |
自动增稳飞机操稳特性的快速评估;张帅等;《江苏航空》;20081231;第2-5页 * |
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Inventor after: Wang Haifeng Inventor after: Tie Yujia Inventor after: Sun Shaoshan Inventor after: Li Xianzhi Inventor after: Tao Chenggang Inventor after: Gao Huiqin Inventor before: Tie Yujia Inventor before: Sun Shaoshan Inventor before: Li Dao Inventor before: Li Xianzhi Inventor before: Tao Chenggang Inventor before: Gao Huiqin |
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