NDLI: Application of active disturbance rejection control to integrated flight-propulsion control

Content Provider	IEEE Xplore Digital Library
Author	Jian Wang Linshu He Mingwei Sun
Copyright Year	2010
Description	Author affiliation: School of Astronautics, BeiHang University (BUAA), Beijing, 100191, China (Jian Wang; Linshu He) \|\| Department of Automation, Nankai University, Tianjin, 300071, China (Mingwei Sun)
Abstract	Integrated flight-propulsion control (IFPC) in cruise mode is under study for ramjet powered supersonic vehicle. The longitudinal flight control and propulsion control model are built with system disturbance and measurement noise. We propose a decoupling active disturbance rejection control (ADRC) scheme for IFPC design. For velocity control loop, a second-order linear extended state observer (ESO) is used. The altitude control loop includes inner pitch angle control and outer altitude control. Two third-order linear ESOs are applied in the altitude control loop. These ESOs estimate the disturbances on altitude and pitch angle, and their parameters are determined by their bandwidth. Two tracking-differentiators (TD) ensure the transient process of velocity and altitude. The linear combinations of state error feedback are applied. The control design eliminates coupling effects between altitude and velocity and attenuates measurement noise.
Starting Page	2565
Ending Page	2569
File Size	222363
Page Count	5
File Format	PDF
ISBN	9781424451814
DOI	10.1109/CCDC.2010.5498776
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2010-05-26
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	State feedback active disturbance rejection control Control design decoupling Observers Integrated flight-propulsion control Noise measurement Ramjet Power system modeling Vehicles Aerospace control Velocity control Bandwidth Propulsion supersonic
Content Type	Text
Resource Type	Article

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