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.


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    Title :

    Landing Advisor System for Aircrafts


    Contributors:

    Publication date :

    2024-08-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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