HARD LANDING DETECTION

A method and system for detecting a hard landing or other high load event of an aircraft are disclosed. A heuristic algorithm may be used to estimate loads experienced by the aircraft during landing. The heuristic algorithm may use flight parameters and/or measured sensor information to estimate the...

Full description

Saved in:
Bibliographic Details
Main Authors ANDERSON, David M, DAVIS, Christopher L, EARLE, David P, AKDENIZ, Aydin, HAUGSE, Eric D, HAGELIN, Jack S, LEPERE, Jonathan R, REUTER, Richard J
Format Patent
LanguageEnglish
French
German
Published 27.03.2019
Subjects
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
CONTROL OR REGULATING SYSTEMS IN GENERAL
CONTROLLING
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
FUNCTIONAL ELEMENTS OF SUCH SYSTEMS
HELICOPTERS
MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS
PARACHUTES
PERFORMING OPERATIONS
PHYSICS
REGULATING
TRANSPORTING
Online AccessGet full text

Cover

More Information
Summary:A method and system for detecting a hard landing or other high load event of an aircraft are disclosed. A heuristic algorithm may be used to estimate loads experienced by the aircraft during landing. The heuristic algorithm may use flight parameters and/or measured sensor information to estimate the loads. The heuristic algorithm may be trained by means of analytical loads predictions and/or test measurements. The heuristic algorithm may be updated during operation. This invention may potentially reduce the number of unnecessary structural inspections, and may also limit the scope of any such required inspections.
Bibliography:Application Number: EP20070845005