State-Dependent Riccati-Equation-Based Guidance Law for Impact-Angle-Constrained Trajectories

By Ashwini Ratnoo, Debasish Ghose. 2009

178 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/df17ad6f59da886a002a0dc3eda5d22fcc0651a6

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. Tayfun Çimen

In Computational Mechanics

1. Rajarshi Bardhan
2. Sachit Rao
3. Shashi Ranjan Kumar
4. Tayfun Çimen
5. Debasish Ghose

Citations in the corpus

• Nonsingular Terminal Sliding Mode Guidance with Impact Angle Constraints (2014, background): “In the guidance laws proposed in [15–29], except [27], the estimation of tgo plays a crucial role.”
• Survey of State-Dependent Riccati Equation in Nonlinear Optimal Feedback Control Synthesis (2012, background): “f) The sixth contribution is guidance law development for acceleration-limited [45] and impact-angle constrained [46] trajectories.”
• Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law (2015, methodology): “The guidance laws derived in [22–24,26,29] do not take into account the target’s maneuver in their formulations, BARDHAN AND GHOSE 385”
• Sliding-Mode Guidance and Control for All-Aspect Interceptors with Terminal Angle Constraints (2012, methodology): “In [7], a guidance law for stationary targets has been derived as the solution to a nonlinear regulator problem using the state-dependent Ricatti-equation technique, where the time-varying state-weighting matrix is assumed to be a function of tgo.”