TY  - JOUR
PY  - 2017//
TI  - Integrated guidance and control design of the suicide UCAV for terminal attack
JO  - Journal of Systems Engineering and Electronics
A1  - Zhou, H.
A1  - Zhao, H.
A1  - Huang, H.
A1  - Zhao, X.
SP  - 546
EP  - 555
VL  - 28
IS  - 3
N2  - A novel integrated guidance and control (IGC) design method is proposed to solve problems of low control accuracy for a suicide unmanned combat aerial vehicle (UCAV) in the terminal attack stage. First of all, the IGC system model of the UCAV is built based on the three-channel independent design idea, which reduces the difficulties of designing the controller. Then, IGC control laws are designed using the trajectory linearization control (TLC). A nonlinear disturbance observer (NDO) is introduced to the IGC controller to reject various uncertainties, such as the aerodynamic parameter perturbation and the measurement error interference. The stability of the closed-loop system is proven by using the Lyapunov theorem. The performance of the proposed IGC design method is verified in a terminal attack mission of the suicide UCAV. Finally, simulation results demonstrate the superiority and effectiveness in the aspects of guidance accuracy and system robustness. © 2017 Beijing Institute of Aerospace Information.<p /> <p>Language: en</p>
LA  - en
SN  - 1671-1793
UR  - http://dx.doi.org/10.21629/JSEE.2017.03.14
ID  - ref1
ER  -