Impact Time and Angle Guidance With Sliding Mode Control

By N. Harl, Sivasubramanya Nadar Balakrishnan. IEEE Transactions on Control Systems Technology, 2009

388 citations recorded by the source corpus.

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Impact-Angle-Constrained Suboptimal Model Predictive Static Programming Guidance of Air-to-Ground Missiles (2012, methodology): “More recently, a sliding mode-based impact time and impact angle control has been proposed by Harl and Balakrishnan [14].”
Prescribed-Time Control and Its Latest Developments (2022, methodology): “for stochastic nonlinear systems, where a nonscaling method is used [17], [18], [19]; PT control for nonlinear systems within a liner decay rate [22]; PT control for normal-form systems, where Faà di Bruno’s formula and Bell polynomials are used [23]; frozen-time eigenvalues for PT-stabilized linear”
Generalized Model Predictive Static Programming and Angle-Constrained Guidance of Air-to-Ground Missiles (2014, background): “Most recently, impact-angle-constrained guidance laws have been presented by using slidingmode control [31–33].”
Nonsingular Sliding Mode Guidance for Impact Time Control (2016, methodology): “In [14], a sliding-mode-control-based guidance law is proposed with the impact time and angle constraints.”