Guidance Laws with Finite Time Convergence

By Di Zhou, Sheng Sun, Kok Lay Teo. 2009

281 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/cd5beef839860d7b469c7b66e1e052b0dafc0571

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. Debasish Ghose
2. Sachit Rao
3. Shashi Ranjan Kumar
4. G. Duan
5. Bin Zhou
6. Zongli Lin
7. Rajarshi Bardhan

In Control and Systems Engineering

1. Debasish Ghose
2. Sachit Rao
3. G. Duan
4. Bin Zhou
5. Shashi Ranjan Kumar
6. Zongli Lin
7. Tingshu Hu
8. Shuzhi Sam Ge

Citations in the corpus

• Lyapunov Differential Equation Approach to Elliptical Orbital Rendezvous with Constrained Controls (2011, methodology): “Hence, these efficient equations are the basic tools and foundation in rendezvous (see, for example, [4–8]).”
• Nonsingular Terminal Sliding Mode Guidance with Impact Angle Constraints (2014, background): “The same kind of singularity can also be observed in a guidance law that focuses only on interception with finite time convergence [6], where the guidance law has been derived for maneuvering targets using finite time stability of nonlinear systems and the Lyapunov scalar differential inequality.”