title: Non-singular terminal dynamic surface control based integrated guidance and control design and simulation.
abstract: In this paper, a novel cascade type design model is transformed from the simulation model, which has a broader scope of application, for integrated guidance and control (IGC). A novel non-singular terminal dynamic surface control based IGC method is proposed. It can guarantee the missile with multiple disturbances fast hits the target with high accuracy, while considering the terminal impact angular constraint commendably. And the stability of the closed-loop system is strictly proved. The essence of integrated guidance and control design philosophy is reached that establishing a direct relation between guidance and attitude equations by "intermediate states" and then designing an IGC law for the obtained integrated cascade design model. Finally, a series of simulations and comparisons with a 6-DOF nonlinear missile that includes all aerodynamic effects are demonstrated to illustrate the effectiveness and advantage of the proposed IGC method.
authors.affiliation: State Key Laboratory of Virtual Reality Technology and Systems, Beihang University, Beijing 100191, China; School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China; Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing 100191, China.
authors.forename: Zhang
authors.initials: Z
authors.lastname: Cong
authors.affiliation: State Key Laboratory of Virtual Reality Technology and Systems, Beihang University, Beijing 100191, China; School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China; Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing 100191, China.
authors.forename: Wu
authors.initials: W
authors.lastname: Yun-Jie
keywords: Dynamic surface control (DSC); Integrated guidance and control (IGC); Non-singular terminal sliding mode control (NTSMC); Simulations