Title :
Effects of time-to-go errors on performance of optimal guidance laws
Author :
Chang-Hun Lee ; Tae-Hun Kim ; Min-Jea Tahk
Author_Institution :
Agency for Defense Dev., Daejeon, South Korea
Abstract :
This paper describes the sensitivity analysis concerning time-to-go estimation error for the class of optimal impact angle control guidance laws under a stationary or a slowly moving target. First, in this paper, the closed-form solutions of those guidance laws for a lag-free system are determined. Then, we derive the explicit expressions of the terminal errors (i.e., miss distance and impact angle error) in the presence of a constant positive time-to-go estimation error. Based on these results, the guidance parameters that can help reduce the sensitivity to time-to-go estimation error are identified. Additionally, the terminal performance of the presented optimal impact angle guidance laws is evaluated from the standpoint of robustness against the time-to-go estimation errors. Numbers of linear homing simulations are also performed to confirm the analysis results.
Keywords :
aerospace control; optimal control; spatial variables control; closed form solutions; impact angle error; lag-free system; miss distance; optimal guidance laws; optimal impact angle control guidance laws; sensitivity analysis; slowly moving target; terminal error; time-to-go estimation error; Closed-form solutions; Differential equations; Estimation error; Kinematics; Missiles; Sensitivity analysis;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.2015.150163