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30 sty 2021 · In this paper, a sequential convex programming algorithm is developed for time-varying PN guidance law design under impact time and impact angle constraints, as well as field-of-view and acceleration limits.
6 maj 2024 · In this paper, a new guidance strategy is proposed for achieving precise control of time-varying velocity aircraft with impact time and angle constraints.
26 wrz 2022 · [29] Hu Q., Cao R., Han T. and Xin M., “ Field-of-View Limited Guidance with Impact Angle Constraint and Feasibility Analysis,” Aerospace Science and Technology, Vol. 114, July 2021, Paper 106753.
6 maj 2022 · As described in Sect. 3.1, we can derive guidance laws that satisfy the zero miss distance and impact angle at the terminal time with respect to arbitrary weighting functions. To minimize the control energy, we can set the weighting function as \(W(\tau ) = 1\). Therefore, the OGL can be defined as follows:
22 lut 2018 · In this paper, a new guidance strategy is proposed for intercepting stationary and constant-velocity moving targets with desired impact time and angle via a virtual target approach, subject to nonlinear engagement kinematics and lateral-acceleration limits. The guidance procedure is divided into two stages by introducing a virtual target.
24 lut 2019 · This guidance law enables missiles with different initial conditions to attack targets simultaneously, and it can also precisely satisfy the terminal impact angle conditions in both flight-path angle and heading angle.
1 sty 2019 · A new guidance law with both impact time and impact angle constraints is proposed in this paper. We first simplify missile dynamics under small heading error approximation, and derive an optimal guidance law with impact angle constraint against a stationary target.
