1. WO2026174470 - AIRCRAFT CONTROL METHOD AND RELATED DEVICE AND SYSTEM

Publication Number WO/2026/174470

Publication Date 27.08.2026

International Application No. PCT/CN2025/078123

International Filing Date 19.02.2025

IPC

G05D 1/82 2024.1

G	PHYSICS
05	CONTROLLING; REGULATING
D	SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
1	Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
80	Arrangements for reacting to or preventing system or operator failure
82	Limited authority control, e.g. enforcing a flight envelope

G05D 1/82 2024.1

G	PHYSICS
05	CONTROLLING; REGULATING
D	SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
1	Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
80	Arrangements for reacting to or preventing system or operator failure
82	Limited authority control, e.g. enforcing a flight envelope

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Applicants

• 深圳市闪至科技有限公司 SZ SHANZHI TECHNOLOGY CO., LTD. [CN]/[CN]

Inventors

• 莫帮杰 MO, Bangjie

Agents

• 北京博思佳知识产权代理有限公司 BEIJING BESTIPR INTELLECTUAL PROPERTY LAW CORPORATION

Priority Data

Publication Language Chinese (zh)

Filing Language Chinese (zh)

Designated States

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AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CV, CZ, DE, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IQ, IR, IS, IT, JM, JO, JP, KE, KG, KH, KN, KP, KR, KW, KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, MG, MK, MN, MU, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, SD, SE, SG, SK, SL, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UY, UZ, VC, VN, WS, ZA, ZM, ZW
African Regional Intellectual Property Organization (ARIPO) (BW, CV, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SC, SD, SL, ST, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Organization (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, ME, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG)

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Title

(EN) AIRCRAFT CONTROL METHOD AND RELATED DEVICE AND SYSTEM

(FR) PROCÉDÉ DE COMMANDE D'AÉRONEF ET DISPOSITIF ET SYSTÈME ASSOCIÉS

(ZH) 飞行器的控制方法及相关设备和系统

Abstract

(EN) An aircraft control method and a related device and system. An aircraft (10) carries a mounting mechanism (20), and the mounting mechanism (20) is used for loading and unloading a payload. The method comprises: in response to an aircraft (10) being in a payload loading/unloading state, restricting a control authority of a control terminal (30) of the aircraft over the aircraft (10) (S11); and in response to the aircraft (10) exiting the payload loading/unloading state, restoring the control authority of the control terminal (30) of the aircraft (10) over the aircraft (10) (S12), wherein the aircraft (10) is located in the air.

(FR) L'invention concerne un procédé de commande d'aéronef, ainsi qu'un dispositif et un système associés. Un aéronef (10) transporte un mécanisme de montage (20), et le mécanisme de montage (20) est utilisé pour charger et décharger une charge utile. Le procédé consiste à : en réponse au fait qu'un un aéronef (10) est dans un état de chargement/déchargement de charge utile, restreindre une autorité de commande d'une borne de commande (30) de l'aéronef sur l'aéronef (10) (S11) ; et en réponse à la sortie de l'aéronef (10) de l'état de chargement/déchargement de charge utile, restaurer l'autorité de commande de la borne de commande (30) de l'aéronef (10) sur l'aéronef (10) (S12), l'aéronef (10) étant situé dans l'air.

(ZH) 一种飞行器的控制方法及相关设备和系统，飞行器(10)搭载有挂载机构(20)，挂载机构(20)用于装卸载荷，方法包括：响应于飞行器(10)处于载荷装卸状态，限制飞行器的控制终端(30)对飞行器(10)的控制权限(S11)；以及响应于飞行器(10)退出载荷装卸状态，恢复飞行器(10)的控制终端(30)对飞行器(10)的控制权限(S12)；其中，飞行器(10)位于空中。

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