Linear Quadratic Guidance Laws for Imposing a Terminal Intercept Angle

By Vitaly Shaferman, Tal Shima. 2008

270 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Statistical and Nonlinear Physics

View Paper: https://www.semanticscholar.org/paper/89c0aed8165ab93394e17d7a34f62a3787d5c52e

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Rajarshi Bardhan
2. Debasish Ghose
3. Sachit Rao
4. Shashi Ranjan Kumar
5. Tae-Hun Kim
6. Bong-Gyun Park
7. Arnab Maity
8. Min-Jae Tahk

In Statistical and Nonlinear Physics

1. Debasish Ghose
2. Rajarshi Bardhan
3. Sachit Rao
4. Shashi Ranjan Kumar
5. Tae-Hun Kim
6. Bong-Gyun Park
7. Radhakant Padhi
8. Harshal B. Oza

Citations in the corpus

• 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].”
• Sliding-Mode Guidance and Control for All-Aspect Interceptors with Terminal Angle Constraints (2012, background): “In both [12,13], linear engagement dynamics are used.”
• Optimal Impact Angle Control Guidance Law Based on Linearization About Collision Triangle (2014, background): “This is why some papers just assume before linearization that the end game is initiated with a collision triangle satisfying closely the impact angle requirement [9].”
• Bias-Shaping Method for Biased Proportional Navigation with Terminal-Angle Constraint (2013, methodology): “Using the Schwartz inequality and differential game theory, terminal-impact-angle-constrained guidance laws for maneuvering targets were developed in [4,5], respectively.”
• Impact-Angle-Constrained Suboptimal Model Predictive Static Programming Guidance of Air-to-Ground Missiles (2012, background): “Shaferman and Shima [9] have also proposed angle constrained guidance schemes based on optimal control and differential game theory.”
• Nonsingular Terminal Sliding Mode Guidance with Impact Angle Constraints (2014, background): “The guidance laws in [25,26] are designed for maneuvering targets.”
• Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law (2015, methodology): “Another quantity related to impact-angle-constrained guidance is defined here in line with [17].”