WO2026126127 - OMNIDIRECTIONAL MULTI-ROTOR AERIAL VEHICLE
National phase entry:
Publication Number
WO/2026/126127
Publication Date
18.06.2026
International Application No.
PCT/IB2025/062692
International Filing Date
10.12.2025
Title **
[English]
OMNIDIRECTIONAL MULTI-ROTOR AERIAL VEHICLE
[French]
VÉHICULE AÉRIEN À MULTIPLES ROTORS OMNIDIRECTIONNEL
Applicants **
NEW YORK UNIVERSITY IN ABU DHABI CORPORATION
Inventors
HAMANDI, Mahmoud
ALI, Abdullah Mohamed
TZES, Anthony
KYRIAKOPOULOS, Konstantinos
KHORRAMI, Farshad
Priority Data
63/730,877
11.12.2024
US
Application details
| Total Number of Claims/PCT | * |
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| Number of Multi-Dependent Claims | * |
| Number of Drawings | * |
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International Searching Authority |
MOIP
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| Recordal of a Change of the Applicant's Name/Address |
Change of Applicant's Name and Address
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| Type of Assignment |
The Standard Agent's Assignment
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| Applicant's Legal Status |
Legal Entity
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| Entry into National Phase under |
Chapter I
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| Patent Delivery |
Send the Letters Patent by Courier
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| Translation |
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* The data is based on automatic recognition. Please verify and amend if necessary.
** IP-Coster compiles data from publicly available sources. If this data includes your personal information, you can contact us to request its removal.
Quotation for National Phase entry
| Country | Stages | Total | |
|---|---|---|---|
| China | Filing, Examination, Granting | 2431 | |
| EPO | Filing, Examination, Granting | 16378 | |
| Japan | Filing, Examination, Granting | 2431 | |
| South Korea | Filing, Examination, Granting | 2043 | |
| USA | Filing, Examination, Granting | 6740 |
Total:
30,023
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Abstract[English]
Described herein is an omnidirectional multi-rotor aerial vehicle system. The system includes a main body and a plurality of arms. The system includes a plurality of propellers. Each of the plurality of propellers are coupled to an end of a respective arm of the plurality of arms and are configured to generate a force and a moment. The system includes a plurality of motors, each communicatively coupled to a respective propeller and configured to rotate the respective propeller. The system includes a controller communicatively coupled to the plurality of motors. The controller includes one or more processors to compute a propeller action for each propeller. The propeller action is computed based upon a desired position of the system and a weight of the system.[French]
L'invention concerne un système de véhicule aérien à rotors multiples omnidirectionnel. Le système comprend un corps principal et une pluralité de bras. Le système comporte une pluralité d'hélices. Chacune de la pluralité d'hélices est couplée à une extrémité d'un bras respectif de la pluralité de bras et est conçue pour générer une force et un moment. Le système comprend une pluralité de moteurs, chacun couplé en communication à une hélice respective et conçu pour faire tourner l'hélice respective. Le système présente un dispositif de commande couplé en communication à la pluralité de moteurs. Le dispositif de commande comprend un ou plusieurs processeurs pour calculer une action d'hélice pour chaque hélice. L'action d'hélice est calculée sur la base d'une position souhaitée du système et d'un poids du système.