DocumentCode
3219944
Title
Model predictive control for path following of stratospheric airship with magnitude and rate constrains of rudder
Author
Ming Zhu ; Shuaixian Yu ; Zewei Zheng
Author_Institution
Sch. of Aeronaut. Sci. & Eng., Beihang Univ., Beijing, China
fYear
2015
fDate
23-25 May 2015
Firstpage
3444
Lastpage
3449
Abstract
This paper presents an effective path following control method for an under-actuated stratospheric airship with rudder constraints. Firstly, dynamic model of the stratospheric airship is described by kinematics and dynamics equations which the controller design is based on. During the movement of stratospheric airship, magnitude and rate of rudder are constrained. Then, the path following controller for the stratospheric airship with magnitude and rate constrains of rudder is designed based on the Guidance-Based Path Following (GBPF) principle and the Model Predictive Control (MPC) theory. The MPC scheme can handle constraints explicitly. Finally, the simulation results are presented to illustrate that the stratospheric airship can converge to a desired path while the inputs and input increments are less than the limits.
Keywords
aerospace components; aircraft control; path planning; predictive control; vehicle dynamics; GBPF; MPC scheme; dynamics equations; guidance-based path following principle; kinematics equations; magnitude constrains; model predictive control theory; path following control method; rate constrains; rudder constraints; under-actuated stratospheric airship; Aerodynamics; Atmospheric modeling; Cost function; Kinematics; Mathematical model; Propellers; Trajectory; Guidance-Based Path following; Model Predictive Control; Rudder Constraints; Stratospheric Airship;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location
Qingdao
Print_ISBN
978-1-4799-7016-2
Type
conf
DOI
10.1109/CCDC.2015.7162518
Filename
7162518
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