论文部分内容阅读
This article analyzes the problem about the missile overload requirement in a homing terminal guidance under various engagement scenarios.An augmented proportional navigation guidance(APNG) model is introduced on the basis of linear kinematics.To analyze the peak-to-peak performance of the terminal guidance system,a new finite time L1 performance measure for a linear time-varying(LTV) continuous system is proposed.Then,according to the idea of the adjoint system,a novel method for computing the L1 norm of a linear continuous system is first derived.Within the finite time L1 framework,the quantitative relation between the guidance loop dynamics and the maximum missile-target maneuver ratio is offered.This relation is expressed in the form of graphs and formulas that can be used to synthesize some of the major subsystem specifications for the missile guidance system.The illustrative examples show that a significant performance improvement is achieved with the proposed guidance loop dynamics.
This article analyzes the problem about the missile overload requirement in a homing terminal guidance under various engagement scenarios. An augmented pilot guidance (APNG) model is introduced on the basis of linear kinematics. To analyze the peak-to-peak performance of the terminal guidance system, a new finite time L1 performance measure for a linear time-varying (LTV) continuous system is proposed. Chen, according to the idea of the adjoint system, a novel method for computing the L1 norm of a linear continuous system is first derived.Within the finite time L1 framework, the quantitative relation between the guidance loop dynamics and the maximum missile-target maneuver ratio is offered. This relation is expressed in the form of graphs and formulas that can be used to synthesize some of the major subsystem specifications for the missile guidance system. The examples examples show that a significant performance improvement is achieved with the proposed guidance loop dynam ics.