Sliding-Mode Guidance and Control for All-Aspect Interceptors with Terminal Angle Constraints

By Shashi Ranjan Kumar, Sachit Rao, Debasish Ghose. 2012

322 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Statistical and Nonlinear Physics

View Paper: https://www.semanticscholar.org/paper/713d0cec9b87dd7a7e52c302b307072b20328cd7

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 Statistical and Nonlinear Physics

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

Citations in the corpus

• Switched-Gain Guidance for Impact Angle Control Under Physical Constraints (2015, unknown): “A sliding-mode separated guidance and control approach is formulated in [21], where the guidance command has two components for reaching and remaining on the sliding surface, respectively.”
• 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].”
• Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law (2015, methodology): “The problem of singularity at the terminal instant in [31] was later removed in [32] using nonsingular terminal sliding mode control theory.”