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:
Jul. 28, 2026

Filed:

Jan. 03, 2025
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 1/656 (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 1/00 (2024.01); G05D 1/46 (2024.01); G05D 1/81 (2024.01);
U.S. Cl.
CPC ...
G05D 1/665 (2024.01); 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

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.


Find Patent Forward Citations

Loading…