Impact-Angle-Constrained Suboptimal Model Predictive Static Programming Guidance of Air-to-Ground Missiles

By Harshal B. Oza, Radhakant Padhi. 2012

163 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Philosophy

View Paper: https://www.semanticscholar.org/paper/5fa581c495de967c02a2acc4f66cedf67bf6e884

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. Arnab Maity
4. Radhakant Padhi
5. Harshal B. Oza
6. Koray S. Erer
7. Raziye Tekin

In Philosophy

1. Rajarshi Bardhan
2. Debasish Ghose
3. Arnab Maity
4. Radhakant Padhi
5. Harshal B. Oza

Citations in the corpus

• Generalized Model Predictive Static Programming and Angle-Constrained Guidance of Air-to-Ground Missiles (2014, methodology): “Even though it is applicable only to a class of optimal control problems in a strict mathematical sense, it is capable enough to address many complex real-life problems such as the ballisticmissile guidance problem [19], reentry guidance problem of reusable launch vehicles [22,23], and angle-constra”
• Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law (2015, methodology): “Guidance laws based on MPSP and its variant were presented in [27,28], respectively, for solving a finite-horizon nonlinear optimal control problem with hard terminal constraints andwere applied to an impact-angle-constrained problem against a stationary or slow-moving ground target.”