This paper presents a new noncertainty-equivalent adaptive control system for the control of
a missile based on the immersion-and-invariance approach. The mathematical model of the …

This paper proposes the use of Legendre pseudospectral method (PSM) to obtain the
optimal guidance strategy for a two-dimensional interceptor problem. An optimal control …

This paper presents a new robust design for the longitudinal autopilot of a tail-controlled,
skid-to-turn missile based on equivalent-input-disturbance (EID) and generalized extended …

Purpose The purpose of this paper is to design an adaptive nonlinear controller for a
nonlinear system of integrated guidance and control. Design/methodology/approach A …

拖拉机线控液压转向系统采用的单杆液压缸具有非对称性, 为了提高转向系统的控制精度,
提出了双通道PID (proportional integral derivative) 控制方法, 对液压缸活塞杆伸出和缩回的 …

In this paper, a new nonlinear H infin control technique, called thetas-D H infin method, is
employed to design a missile longitudinal autopilot. The thetas-D H infin design has the …

HANSON1 details several past launch vehicle failure forms across the globe and the
reasons for the test format of the NASA Marshall Spaceflight Center (MSFC) reusable launch …

Formation control of multiple spacecraft flying in deep space about the L2 libration point is
investigated. Dynamics of the spacecraft is formulated as a circular restricted three-body …

Теоретические основы решения линейно-квадратических задач в ряде случаев могут
быть применены при синтезе управляющих воздействий для нелинейных систем …