Calculation method for tilting corridor of tilting quadrotor aircraft with constant speed and periodic variable pitch
A tilting quadrotor, cyclic pitch change technology, applied in computing, computer-aided design, instruments, etc., to achieve the effect of small body waste resistance, safe tilting, and maximum body waste resistance
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0083] In order to facilitate the understanding of those skilled in the art, the present invention will be further described below in conjunction with examples and accompanying drawings, and the contents mentioned in the implementation modes are not intended to limit the present invention.
[0084] refer to figure 1 As shown, a method for calculating the tilting corridor of a tilting quadrotor aircraft with a fixed speed and a periodic variable pitch of the present invention includes the following steps:
[0085] 1) Establish the flight mechanics model of each component of the aircraft, transform all forces and moments into the body shaft system, and establish a six-degree-of-freedom balance equation;
[0086] 2) Select the tilting control mode: constant speed with period variable pitch control;
[0087] 3) Solve the upper and lower boundaries of the pitch angle with the wing lift characteristic as the limiting factor; optimize the trim solution to obtain the control amount a...
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