Piecewise Trajectory and Angle Constraint Based Fractional-order Sliding Mode Control
Author:
Affiliation:
1. Beijing Key Laboratory of High Dynamic Navigation Technology, Beijing Information Science and Technology University, Beijing, China
2. School of Aerospace Engineering, Beijing Institute of Technology, China
Funder
National Key Research & De- velopment Program
National Natural Science Foundation of China
Project of Construction and Support for high-level Innovative Teams of Beijing Municipal Institutions
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Aerospace Engineering
Link
http://xplorestaging.ieee.org/ielx7/7/7778228/10144279.pdf?arnumber=10144279
Reference31 articles.
1. Chattering-free fault-tolerant attitude control with fast fixed-time convergence for flexible spacecraft;esmaeilzadeh;Int J Control Automat Syst,2020
2. Integrated Higher-Order Sliding Mode Guidance and Autopilot for Dual Control Missiles
3. Fractional Order Calculus: Basic Concepts and Engineering Applications
4. Optimality of Error Dynamics in Missile Guidance Problems
5. Finite-Time Stability of Continuous Autonomous Systems
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