Optimal Guidance Laws with Terminal Impact Angle Constraint

By Chang-Kyung Ryoo, Hangju Cho, Min-Jae Tahk. 2005

526 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Statistical and Nonlinear Physics

View Paper: https://www.semanticscholar.org/paper/04e1f0dc5bf0e93eaf0b04acdf9b21c529e9d2d1

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In Aerospace Engineering

In Computational Mechanics

In Statistical and Nonlinear Physics

Citations in the corpus

Nonsingular Sliding Mode Guidance for Impact Time Control (2016, background): “Although a number of papers considering IACG have been published [2–8], only a few papers related to ITCG is available in open literature.”
Integral LOS Path Following for Curved Paths Based on a Monotone Cubic Hermite Spline Parametrization (2014, background): “Optimal methods have also appeared in the literature, for more details, the reader is referred to [23] and [24].”
Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law (2015, methodology): “But in [12], time-to-go estimate for an impact-angle-constrained optimal guidance law was derived assuming a stationary or slow-moving target; hence, those time-togo estimates cannot be used against maneuvering targets.”
Composite Guidance Scheme for Impact Angle Control Against a Nonmaneuvering Moving Target (2016, background): “[2] proposed a pure energy optimal guidance law with impact angle constraint.”
Bias-Shaping Method for Biased Proportional Navigation with Terminal-Angle Constraint (2013, background): “In [2], an energy-optimal impact-angle control lawwas proposed by solving the linear quadratic optimal control problem with arbitrary missile dynamics.”
Generalized Model Predictive Static Programming and Angle-Constrained Guidance of Air-to-Ground Missiles (2014, background): “There have been several impact-angle-constrained guidance schemes (most of them in the two dimensional setting), and some of these are in fact based on the optimal control theory [25–29].”
Switched-Gain Guidance for Impact Angle Control Under Physical Constraints (2015, methodology): “Linear formulations for derivation are used in [1,2,5,7–12].”
Impact-Angle-Constrained Suboptimal Model Predictive Static Programming Guidance of Air-to-Ground Missiles (2012, background): “[4], where the lateral acceleration demand is computed for constant speedmissiles that use minimum control energy.”
Linear Quadratic Guidance Laws for Imposing a Terminal Intercept Angle (2008, methodology): “(12), but amore accurate tgo estimation might be needed, such as the one presented in [3].”
Nonsingular Terminal Sliding Mode Guidance with Impact Angle Constraints (2014, methodology): “In the guidance laws proposed in [15–29], except [27], the estimation of tgo plays a crucial role.”