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
Link To Document :
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