Missile Autopilot Controlled by Aerodynamic Lift and Divert Thrusters via Second-Order Sliding Mode

IFAC Proceedings Volumes
doi 10.3182/20050703-6-cz-1902.01994
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Elsevier BV

Related search

Second-Order Sliding Mode Guidance Law Considering Second-Order Dynamics of Autopilot

Journal of Control Science and Engineering
Electronic EngineeringSimulationComputer Science ApplicationsElectricalModeling
2019English

Autopilot for a Nonlinear Non-Minimum Phase Tail-Controlled Missile

2014English

A Second Order Sliding Mode Differentiator With a Variable Exponent

2017English

On Modified Second-Order Sliding Mode Synchronization of Two Different Fractional Order Hyperchaotic Systems

International Journal of Multimedia and Ubiquitous Engineering
Computer Science
2015English

Fuzzy Second Order Sliding Mode Control of a Unified Power Flow Controller

Electrical Engineering & Electromechanics
2019English

Adaptive Fuzzy Sliding-Mode Attitude Controller Design for Spacecrafts With Thrusters

2012English

Output Feedback Control: A Robust Solution Based on Second Order Sliding Mode

IFAC Proceedings Volumes
2008English

Second Order Sliding Mode Control of the Output Voltage Tracking an Matrix Converter

Bulletin of NTU "Kharkiv Polytechnic Institute" Series: Electrical Machines and Electromechanical Energy Conversion
2019English

Aerodynamic Shape Optimization System of a Canard-Controlled Missile Using Trajectory-Dependent Aerodynamic Coefficients

Journal of Spacecraft and Rockets
SpacePlanetary ScienceAerospace Engineering
2012English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy