Sliding mode–based simultaneous control of impact angle and impact time

Abstract

In this article, a sliding mode control–based nonlinear guidance scheme for controlling both impact angle and impact time simultaneously is proposed. The problem of impact angle control is first transformed to that of controlling line-of-sight angle and its rate, while the requirement of impact time is achieved by tracking the desired time-to-go. The chosen time-to-go estimate accounts for the curvature required to meet the impact angle requirements toward the target interception. In order to satisfy both of these terminal constraints, the sliding surface is defined as a combination of impact time error and the variable pertaining to the errors in line-of-sight angle and its rate, with appropriate gains assigned to them. The interceptor first performs necessary maneuvers to meet the impact time requirements and then steers its course to achieve the target interception at a desired impact angle. The guidance law is initially derived using nonlinear engagement kinematics against stationary targets and then extended to cater to constant velocity targets using the concept of predicted interception point. Numerical simulations are performed to validate the efficacy of the proposed guidance scheme for various initial engagement geometries. The performance of the proposed guidance scheme is also compared with those of the existing guidance laws and shown to be superior.

Cubature Kalman Filters Model Predictive Static Programming Guidance Method with Impact Time and Angle Constraints Considering Modeling Errors

“…Yan [16] proposed a computational geometry guidance against stationary targets, satisfying the constraints by iterating parameters of the geometry curve. Majumder [17] proposed a sliding-mode-control-based nonlinear guidance scheme for controlling both impact angle and impact time simultaneously. Liu [18] designed an adaptive sliding mode ITACG method, increasing its adaptability and robustness.…”

“…In Refs. [8][9][10][11][12][13][14][15][16][17][18][19], the guidance methods rely on time-to-go or range-to-go estimation. However, the estimation is difficult because of the uncontrollable varying velocity.…”

Sliding mode control based impact angle constrained guidance with predefined convergence time

“…For most scenarios, the engagement duration is finite and thus the guidance systems are expected to satisfy the desired performance within a finite-time. [4][5][6][7][8][9] The finite-time convergence of the controlled guidance variables to the origin is desirable not only because of the faster convergence, but also due to the expectation that such schemes perform better in the presence of uncertainties and disturbances. 10,11 There have been numerous guidance schemes based on proportional navigation (PN) and its variants 12,13 to ensure the target interception within a finite time.…”