An indication to perform a recovery action, including by deploying a first and second parachute canopy is output. Sensor data, which includes parachute canopy state information associated with the first parachute canopy and the second parachute canopy, is received from a sensor. It is determined, based at least in part on the sensor data, whether to generate a control signal with a value associated with maneuvering the aircraft into a nose-up position. If the parachute canopy state information indicates the first parachute canopy is collapsed and the second is inflated, the control signal is generated with the value associated with maneuvering the aircraft into the nose-up position. A load on the second parachute canopy is reduced if the aircraft is in the nose-up position compared to the aircraft being in a nose-down position. The control signal is output.


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    Title :

    AUTOMATED AIRCRAFT RECOVERY SYSTEM


    Contributors:

    Publication date :

    2025-05-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U



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