TY - GEN
T1 - Longitudinal attitude control of a hypersonic vehicle with angle of attack constraints
AU - Zhikai, Zhang
AU - Guangren, Duan
AU - Mingzhe, Hou
N1 - Publisher Copyright:
© 2015 IEEE.
PY - 2015/9/8
Y1 - 2015/9/8
N2 - An adaptive dynamic surface control algorithm is proposed for longitudinal attitude of the hypersonic vehicle in the presence of angle of attack constraints. The angle of attack constraints are firstly converted into the tracking error constraints, and then a weighted performance function and an error transformation technique are introduced, which guarantee a prescribed performance of tracking error as well as prevent the angle of attack from transgressing the constraints, and the original nonlinear system with constrained tracking error is transformed into an equivalent unconstrained one. An adaptive dynamic surface control algorithm is subsequently proposed to stabilize this transformed error system. It is proved that asymptotic tracking of the longitudinal attitude is achieved without violation of the angle of attack constraints, and all the other signals in the closed loop are uniformly ultimately bounded. The Monte-Carlo simulation results show the effectiveness of the proposed method.
AB - An adaptive dynamic surface control algorithm is proposed for longitudinal attitude of the hypersonic vehicle in the presence of angle of attack constraints. The angle of attack constraints are firstly converted into the tracking error constraints, and then a weighted performance function and an error transformation technique are introduced, which guarantee a prescribed performance of tracking error as well as prevent the angle of attack from transgressing the constraints, and the original nonlinear system with constrained tracking error is transformed into an equivalent unconstrained one. An adaptive dynamic surface control algorithm is subsequently proposed to stabilize this transformed error system. It is proved that asymptotic tracking of the longitudinal attitude is achieved without violation of the angle of attack constraints, and all the other signals in the closed loop are uniformly ultimately bounded. The Monte-Carlo simulation results show the effectiveness of the proposed method.
KW - adaptive dynamic surface control
KW - angle of attack constraints
KW - error transformation
KW - hypersonic vehicle longitudinal attitude control
UR - https://www.scopus.com/pages/publications/84957687815
U2 - 10.1109/ASCC.2015.7244862
DO - 10.1109/ASCC.2015.7244862
M3 - 会议稿件
AN - SCOPUS:84957687815
T3 - 2015 10th Asian Control Conference: Emerging Control Techniques for a Sustainable World, ASCC 2015
BT - 2015 10th Asian Control Conference
A2 - Selamat, Hazlina
A2 - Ramli, Hafiz Rashidi Haruna
A2 - Faudzi, Ahmad Athif Mohd
A2 - Rahman, Ribhan Zafira Abdul
A2 - Ishak, Asnor Juraiza
A2 - Soh, Azura Che
A2 - Ahmad, Siti Anom
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 10th Asian Control Conference, ASCC 2015
Y2 - 31 May 2015 through 3 June 2015
ER -