CN103076806B - 三回路自动驾驶仪控制参数一体化解析整定方法 - Google Patents
三回路自动驾驶仪控制参数一体化解析整定方法 Download PDFInfo
- Publication number
- CN103076806B CN103076806B CN201110329422.XA CN201110329422A CN103076806B CN 103076806 B CN103076806 B CN 103076806B CN 201110329422 A CN201110329422 A CN 201110329422A CN 103076806 B CN103076806 B CN 103076806B
- Authority
- CN
- China
- Prior art keywords
- loop
- flight vehicle
- angular velocity
- guided flight
- transfer function
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Description
Claims (5)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201110329422.XA CN103076806B (zh) | 2011-10-26 | 2011-10-26 | 三回路自动驾驶仪控制参数一体化解析整定方法 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201110329422.XA CN103076806B (zh) | 2011-10-26 | 2011-10-26 | 三回路自动驾驶仪控制参数一体化解析整定方法 |
Publications (2)
Publication Number | Publication Date |
---|---|
CN103076806A CN103076806A (zh) | 2013-05-01 |
CN103076806B true CN103076806B (zh) | 2015-03-25 |
Family
ID=48153373
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201110329422.XA Expired - Fee Related CN103076806B (zh) | 2011-10-26 | 2011-10-26 | 三回路自动驾驶仪控制参数一体化解析整定方法 |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN103076806B (zh) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103353759A (zh) * | 2013-06-25 | 2013-10-16 | 西安交通大学 | 一种基于cdm的导弹自动驾驶仪设计方法 |
CN104133477B (zh) * | 2014-04-17 | 2016-10-26 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种可以实现瞬态抑制的调效控制律指令控制方法 |
CN104155988B (zh) * | 2014-08-12 | 2015-05-20 | 北京航天自动控制研究所 | 飞行器的多通道姿态控制器 |
CN104567545B (zh) * | 2014-10-30 | 2016-08-24 | 中国运载火箭技术研究院 | Rlv大气层内主动段的制导方法 |
CN105159311B (zh) * | 2015-09-14 | 2018-01-05 | 湖北航天技术研究院总体设计所 | 一种用于捷联导引头的自动驾驶仪的设计方法 |
CN105353761B (zh) * | 2015-12-02 | 2018-06-12 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | 一种飞机的速度控制方法及装置 |
CN108763772B (zh) * | 2018-05-30 | 2022-10-21 | 河北清华发展研究院 | 一种固定翼无人机纵向姿态控制器设计方法 |
CN109270840B (zh) * | 2018-09-28 | 2024-05-17 | 四川航天系统工程研究所 | 一种导弹控制系统时变校正网络离散化方法 |
CN109782809A (zh) * | 2019-03-14 | 2019-05-21 | 中国人民解放军陆军工程大学 | 一种考虑自动驾驶仪二阶动态特性的新型导引律 |
CN109901390A (zh) * | 2019-03-14 | 2019-06-18 | 中国人民解放军陆军工程大学 | 一种考虑自动驾驶仪二阶动态特性的二阶滑模导引律 |
CN110456781B (zh) * | 2019-09-16 | 2021-08-24 | 桂林航天工业学院 | 一种飞行器控制系统的空间稳定性分析方法 |
CN111832115B (zh) * | 2020-06-02 | 2023-12-19 | 哈尔滨工业大学(深圳)(哈尔滨工业大学深圳科技创新研究院) | 对称迟后-超前校正的一体化频率设计方法 |
CN111895864B (zh) * | 2020-08-06 | 2022-05-10 | 西安睿高测控技术有限公司 | 一种无加速度计的卫星制导弹药的过载驾驶仪构建方法 |
CN111949043B (zh) * | 2020-08-07 | 2024-02-23 | 上海航天控制技术研究所 | 一种基于姿态角速度判别的启控时刻在线提取方法 |
CN112925336B (zh) * | 2021-01-15 | 2022-11-22 | 北京电子工程总体研究所 | 一种基于缆绳操纵吊舱的囊体姿态控制回路和方法 |
CN113064443B (zh) * | 2021-03-08 | 2022-10-11 | 北京理工大学 | 增益在线调整方法及使用其的阻尼回路控制方法 |
CN117311376B (zh) * | 2023-11-28 | 2024-03-01 | 北京理工大学 | 一种应用于旋转飞行器的自适应神经网络驾驶方法 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4659035A (en) * | 1985-01-25 | 1987-04-21 | The United States As Represented By The Secretary Of The Navy | Rate estimation by mixing two independent rate signals |
CN101655371B (zh) * | 2009-09-18 | 2012-06-06 | 哈尔滨工程大学 | 一种基于变阻尼系数的惯性导航系统方位信号阻尼方法 |
KR101184625B1 (ko) * | 2010-04-15 | 2012-09-21 | 국방과학연구소 | 비행체의 수직면 직선추종 비행 제어기 설계방법 |
-
2011
- 2011-10-26 CN CN201110329422.XA patent/CN103076806B/zh not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CN103076806A (zh) | 2013-05-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103076806B (zh) | 三回路自动驾驶仪控制参数一体化解析整定方法 | |
Liu et al. | Robust attitude controller design for miniature quadrotors | |
CN105607473B (zh) | 小型无人直升机的姿态误差快速收敛自适应控制方法 | |
US8209069B1 (en) | Aircraft sensor anticipator system | |
CN104266663A (zh) | 一种运动平台光电跟踪系统二级稳定扰动解耦方法 | |
Wael et al. | Robust hybrid control for ballistic missile longitudinal autopilot | |
Niermeyer et al. | Open-loop quadrotor flight dynamics identification in frequency domain via closed-loop flight testing | |
Shao et al. | Input-and-measurement event-triggered control for flexible air-breathing hypersonic vehicles with asymmetric partial-state constraints | |
Cakiroglu et al. | Robust incremental nonlinear dynamic inversion control using angular accelerometer feedback | |
Pashilkar et al. | Adaptive back-stepping neural controller for reconfigurable flight control systems | |
Bierling | Comparative analysis of adaptive control techniques for improved robust performance | |
Li et al. | Angular acceleration estimation-based incremental nonlinear dynamic inversion for robust flight control | |
Sun et al. | Practical solution to attitude control within wide envelope | |
Safwat et al. | Robustness analysis of modified incremental nonlinear dynamic inversion for small UAVs | |
Ding et al. | Disturbance rejection attitude control for a quadrotor: theory and experiment | |
CN113419431A (zh) | 一种基于事件触发的平流层飞艇轨迹跟踪控制方法及系统 | |
Khaligh et al. | A system identification strategy for nonlinear model of small-scale unmanned helicopters | |
Gong et al. | Design of automatic climbing controller for large civil aircraft | |
Li et al. | Enhanced disturbance rejection control based test rocket control system design and validation | |
CN115981357A (zh) | 一种四旋翼无人机前飞模态的控制器参数整定方法及系统 | |
Mukarram et al. | Altitude control of a quadcopter | |
CN113050683A (zh) | 一种基于终端滑模控制的固定时间四旋翼飞行器控制方法 | |
Bouzid et al. | Boosted flight controller for quadrotor navigation under disturbances | |
Smith et al. | Observer-based super-twisting sliding mode control of quadcopters | |
Lorenz | Open-loop reference system for nonlinear control applied to unmanned helicopters |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CB03 | Change of inventor or designer information | ||
CB03 | Change of inventor or designer information |
Inventor after: Guo Hongbo Inventor after: Yang Jie Inventor after: Pu Lige Inventor after: Song Chunji Inventor after: Wang Fei Inventor after: Liu Ning Inventor after: Li Wei Inventor after: Liu Sai Inventor after: Ji Hongjuan Inventor after: Shen Defeng Inventor after: Zhuang Ling Inventor after: Li Lei Inventor after: Shui Yongtao Inventor after: Tang Linka Inventor after: Meng Gang Inventor after: Li Jianxin Inventor after: Pu Zhongjie Inventor after: Chen Hao Inventor before: Guo Hongbo Inventor before: Zhuang Ling |
|
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150325 Termination date: 20171026 |