Method of controlling tilt rotor, apparatus for controlling tilt rotor, and aircraft including the apparatus
US12391363B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Nov 16, 2023 |
| Grant date | Aug 19, 2025 |
| Priority date | — |
| Expiry date | Mar 22, 2044 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D31/12
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An apparatus for controlling a tilt rotor is provided. The apparatus includes a thrust command generator configured to generate a first collective pitch angle based on a throttle command, a rotation speed compensator configured to generate a compensation value based on a rotation speed of the motor, a compensation weight generator configured to generate weight values according to a flight speed, a collective pitch angle command generator configured to generate a collective pitch angle adjustment command of the rotor blade of the motor, based on the first collective pitch angle and a first compensation value being obtained by multiplying the compensation value by a preset conversion ratio and a first weight value, and a motor controller configured to generate a motor control command based on a second compensation value being obtained by multiplying the compensation value by a second weight value and the first collective pitch angle.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.