中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Advanced Quadrotor Takeoff Control Based on Incremental Nonlinear Dynamic Inversion and Integral Extended State Observer

文献类型:会议论文

作者Du, Han(杜晗)1,2; Pu, Zhiqiang(蒲志强)1; Yi, Jianqiang(易建强)1; Qian, Hanbo(钱瀚博)3; Zhiqiang Pu
出版日期2016
会议日期August 8 - August 12, 2016
会议地点Nanjing , China
关键词Quadrotor Incremental Nonlinear Dynamic Inversion Integral Extended State Observer
页码1881 - 1886
英文摘要This paper presents an advanced control scheme
for quadrotor taking off process. Firstly a high-fidelity model is
established, with Coriolis force, gyro effect, and ground effect
taken into account. Then the quadrotor control system is
decoupled into three control loops, which are position loop,
angle loop, and inner loop. Dynamic inversion (DI) is applied to
design control laws for both the position and the angle loops.
Incremental nonlinear dynamic inverse (INDI) control law is
furtherly developed to cope with non-affine form of the inner
loop. To realize disturbance rejection and the measurement
noise attenuation, integral extended state observer (IESO) is
combined in this control scheme. Besides, arranged transient
process technique (ATP) is utilized in the control scheme to
smooth huge-jump desired input and connect different loops
with feasible transient process. Finally, through series of
simulations the effectiveness of the control scheme, as well as
robustness against external disturbances and measurement
noise are validated.
会议录Proceedings of 2016 IEEE Chinese Guidance, Navigation and Control Conference
语种英语
源URL[http://ir.ia.ac.cn/handle/173211/14483]  
专题综合信息系统研究中心_飞行器智能技术
通讯作者Zhiqiang Pu
作者单位1.中国科学院自动化研究所
2.中国科学院大学
3.国家国防科技工业局协作配套中心
推荐引用方式
GB/T 7714
Du, Han,Pu, Zhiqiang,Yi, Jianqiang,et al. Advanced Quadrotor Takeoff Control Based on Incremental Nonlinear Dynamic Inversion and Integral Extended State Observer[C]. 见:. Nanjing , China. August 8 - August 12, 2016.

入库方式: OAI收割

来源:自动化研究所

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