US 11,840,349 B2
Aerial vehicle powering off method and device, and aerial vehicle
Renli Shi, Shenzhen (CN); Xuyang Pan, Shenzhen (CN); Jianyu Song, Shenzhen (CN); and Canlong Lin, Shenzhen (CN)
Assigned to SZ DJI TECHNOLOGY CO., LTD., Shenzhen (CN)
Filed by SZ DJI TECHNOLOGY CO., LTD., Shenzhen (CN)
Filed on May 6, 2021, as Appl. No. 17/314,036.
Application 17/314,036 is a continuation of application No. 16/537,281, filed on Aug. 9, 2019, granted, now 11,001,387.
Application 16/537,281 is a continuation of application No. 15/415,303, filed on Jan. 25, 2017, granted, now 10,414,511, issued on Sep. 17, 2019.
Application 15/415,303 is a continuation of application No. PCT/CN2014/083482, filed on Jul. 31, 2014.
Prior Publication US 2021/0261264 A1, Aug. 26, 2021
Int. Cl. B64D 31/00 (2006.01); G05D 1/06 (2006.01); B64U 50/19 (2023.01); B64U 70/40 (2023.01); B64D 45/04 (2006.01)
CPC B64D 31/00 (2013.01) [B64D 45/04 (2013.01); B64U 50/19 (2023.01); B64U 70/40 (2023.01); G05D 1/0676 (2013.01)] 19 Claims
OG exemplary drawing
 
1. A method for automatically powering off an aerial vehicle comprising:
determining an operating state of the aerial vehicle; and
in response to a determination result that the operating state of the aerial vehicle is a landed state:
determining whether a propulsion output of the aerial vehicle is currently enabled and determining whether an automatic take-off operation indicated by an automatic take-off instruction is currently being performed; and
in response to a triggering condition being satisfied triggering to shut down the propulsion output of the aerial vehicle such that the aerial vehicle completes automatic power off after landing, the triggering condition including determining that the propulsion output is currently enabled and the automatic take-off operation is not currently performed.