Guidance and Control of Missile Interceptor using Second-Order Sliding Modes

By Yuri B. Shtessel, Ilya A. Shkolnikov, Arie Levant. IEEE Transactions on Aerospace and Electronic Systems, 2009

318 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Control and Systems Engineering, Statistical and Nonlinear Physics

View Paper: https://www.semanticscholar.org/paper/4d7200743d5149be285476292f859a039189e6ea

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. Lei Guo
2. Changyin Sun
3. Jinzhi Wang
4. Xianghua Wang
5. Shihua Li

In Control and Systems Engineering

1. Jun Yang
2. Shihua Li
3. Lei Guo
4. Ruiting Bai
5. Changyin Sun
6. Xiaoyan Wu
7. Yong-Xing Chen
8. Jinzhi Wang

In Statistical and Nonlinear Physics

1. Jinzhi Wang
2. Xianghua Wang

Citations in the corpus

• Nonlinear-Disturbance-Observer-Based Robust Flight Control for Airbreathing Hypersonic Vehicles (2013, background): “Inspired from [21]—[23], a nonlinear disturbance observer (NDO) with finite-time convergence property, which provides an adequate way to estimate the disturbances for the AHV system (12), is constructed first”
• Design of a class of new nonlinear disturbance observers based on tracking differentiators for uncertain dynamic systems (2015, background): “High order sliding mode differentiator (SMD) [12-14] is difficult to be implemented due to its need of Lipschitz upper bound of the disturbance’s ith derivative.”
• Partial Integrated Missile Guidance and Control with Finite Time Convergence (2013, methodology): “To overcome this difficulty, the idea of partial IGC with a two-loop controller structure [2,29,30] is used in this paper.”