Finite-time control method for quadrotor aircraft based on hyperbolic tangent-enhanced constant-velocity reaching law and fast terminal sliding surface
A technology of four-rotor aircraft and control method, applied in control/adjustment system, non-electric variable control, three-dimensional position/course control, etc., can solve the problem of accelerating the approach speed of the system to the sliding mode surface and accelerating the approach speed of the approach law , Unable to achieve limited time control and other problems, to achieve the effect of realizing limited time control, increasing approach speed and shortening arrival time
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0073] The present invention will be further described below in conjunction with the accompanying drawings.
[0074] refer to Figure 1-Figure 7 , a finite-time control method for quadrotor aircraft based on hyperbolic tangent-enhanced constant-velocity reaching law and fast terminal sliding surface, including the following steps:
[0075] Step 1, determine the transfer matrix from the body coordinate system based on the quadrotor aircraft to the inertial coordinate system based on the earth;
[0076]
[0077] Among them, ψ, θ, and φ are the yaw angle, pitch angle, and roll angle of the aircraft, respectively, indicating the rotation angle of the aircraft around each axis of the inertial coordinate system in turn, and T ψ represents the transition matrix of ψ, T θ Denotes the transition matrix of θ, T φ Represents the transition matrix of φ;
[0078] Step 2, analyze the quadrotor aircraft dynamics model according to the Newton Euler formula, the process is as follows: ...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com