Landing Advisor System for Aircrafts
    1.
    发明公开

    公开(公告)号:US20240278931A1

    公开(公告)日:2024-08-22

    申请号:US18171364

    申请日:2023-02-19

    IPC分类号: B64D45/04

    CPC分类号: B64D45/04 B64D2045/008

    摘要: A landing adviser system for aircrafts comprising of a main housing, a microcontroller installed within the main housing, an environmental sensor array connected to the main housing, where the environmental sensor array electronically communicates with the microcontroller, a portable power source in the proximity of the main housing, where the portable power source provides electrical power to the microcontroller and the sensor array, a landing data collected by the environmental sensor array, where the landing data is communicated to the microcontroller, and a communication module for communicating the landing data from the microcontroller to the pilot of an aircraft. The environmental sensor array comprises an anemometer, an optical sensor and range finder, a thermometer, a hygrometer, a penetrometer, a gyroscope, and a global positioning system. The system further comprises an external sensor post, a beacon, algorithms for computing wind gusts and turbulence around nearby structures, and a padded carrying case.