TY - JOUR
T1 - Observer-based adaptive sliding mode backstepping output-feedback DSC for spin-stabilized canard-controlled projectiles
AU - SHEN, Yuanchuan
AU - YU, Jianqiao
AU - LUO, Guanchen
AU - AI, Xiaolin
AU - JIA, Zhenyue
AU - CHEN, Fangzheng
N1 - Publisher Copyright:
© 2017
PY - 2017/6
Y1 - 2017/6
N2 - This article presents a complete nonlinear controller design for a class of spin-stabilized canard-controlled projectiles. Uniformly ultimate boundedness and tracking are achieved, exploiting a heavily coupled, bounded uncertain and highly nonlinear model of longitudinal and lateral dynamics. In order to estimate unmeasurable states, an observer is proposed for an augmented multiple-input-multiple-output (MIMO) nonlinear system with an adaptive sliding mode term against the disturbances. Under the frame of a backstepping design, an adaptive sliding mode output-feedback dynamic surface control (DSC) approach is derived recursively by virtue of the estimated states. The DSC technique is adopted to overcome the problem of “explosion of complexity” and relieve the stress of the guidance loop. It is proven that all signals of the MIMO closed-loop system, including the observer and controller, are uniformly ultimately bounded, and the tracking errors converge to an arbitrarily small neighborhood of the origin. Simulation results for the observer and controller are provided to illustrate the feasibility and effectiveness of the proposed approach.
AB - This article presents a complete nonlinear controller design for a class of spin-stabilized canard-controlled projectiles. Uniformly ultimate boundedness and tracking are achieved, exploiting a heavily coupled, bounded uncertain and highly nonlinear model of longitudinal and lateral dynamics. In order to estimate unmeasurable states, an observer is proposed for an augmented multiple-input-multiple-output (MIMO) nonlinear system with an adaptive sliding mode term against the disturbances. Under the frame of a backstepping design, an adaptive sliding mode output-feedback dynamic surface control (DSC) approach is derived recursively by virtue of the estimated states. The DSC technique is adopted to overcome the problem of “explosion of complexity” and relieve the stress of the guidance loop. It is proven that all signals of the MIMO closed-loop system, including the observer and controller, are uniformly ultimately bounded, and the tracking errors converge to an arbitrarily small neighborhood of the origin. Simulation results for the observer and controller are provided to illustrate the feasibility and effectiveness of the proposed approach.
KW - Backstepping
KW - Dynamic surface control technique
KW - Nonlinear systems
KW - Observers
KW - Sliding mode control
KW - Spin-stabilized canard-controlled projectiles
UR - http://www.scopus.com/inward/record.url?scp=85020009257&partnerID=8YFLogxK
U2 - 10.1016/j.cja.2017.01.004
DO - 10.1016/j.cja.2017.01.004
M3 - Article
AN - SCOPUS:85020009257
SN - 1000-9361
VL - 30
SP - 1115
EP - 1126
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 3
ER -