The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 11, 2025

Filed:

Feb. 27, 2024
Applicant:

Kitty Hawk Corporation, Palo Alto, CA (US);

Inventors:

Cameron Robertson, San Mateo, CA (US);

Joseph Roop, Sunnyvale, CA (US);

Todd Reichert, Mountain View, CA (US);

Damon Vander Lind, Alameda, CA (US);

Assignee:

Kitty Hawk Corporation, Palo Alto, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2024.01); B64D 17/54 (2006.01); B64D 17/62 (2006.01); B64D 17/72 (2006.01); B64D 17/80 (2006.01); B64D 45/00 (2006.01); B64U 70/83 (2023.01); G05D 1/46 (2024.01); G05D 1/81 (2024.01);
U.S. Cl.
CPC ...
G05D 1/0061 (2013.01); B64D 17/54 (2013.01); B64D 17/62 (2013.01); B64D 17/80 (2013.01); B64D 45/00 (2013.01); G05D 1/042 (2013.01); G05D 1/0808 (2013.01); G05D 1/46 (2024.01); G05D 1/81 (2024.01); B64D 17/725 (2013.01); B64D 2045/0085 (2013.01); B64U 70/83 (2023.01);
Abstract

Sensor data is received from a sensor where the sensor data includes aircraft state information including an aircraft pitch angle and recovery device state information including which parachute canopies are operational and one or more properties associated with the operational parachute canopies. The parachute canopies are coupled aft of a center of mass. It is determined, based at least in part on the aircraft pitch angle, whether to generate a control signal associated with maneuvering the aircraft into a nose-up position. A recovery action is performed, including by selecting a parachute canopy to be deployed, from the operational parachute canopies and based at least in part on the one or more properties, and deploying the selected parachute canopy, where a load on the selected parachute canopy is reduced in the event the aircraft is in the nose-up position compared to the aircraft being in a nose-down position.


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