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公开(公告)号：US11407509B2
公开(公告)日：2022-08-09
申请号：US16744064
申请日：2020-01-15
Applicant: Wisk Aero LLC
Inventor： Ilan Kroo , Herve Martins-Rivas , Eric Allison
Abstract: In various embodiments, a tilt-wing aircraft includes a fuselage; a first wing tiltably mounted at or near a forward end of the fuselage; and a second wing rotatably mounted to the fuselage at a position aft of the first wing. A first plurality of rotors is mounted on the first wing at locations on or near a leading edge of the first wing, with two or more rotors being mounted on wing portions on each side of the fuselage; and a second plurality of rotors mounted on the second wing at locations on or near a leading edge of the second wing, with two or more rotors being mounted on wing portions on each side of the fuselage. A flight control system generates a set of actuators and associated actuator parameters to achieve desired forces and moments.
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公开(公告)号：US20240367787A1
公开(公告)日：2024-11-07
申请号：US18777420
申请日：2024-07-18
Applicant: Wisk Aero LLC
Inventor： Zouhair Mahboubi , Gabe Hoffmann , Olivier Toupet , Herve Martins-Rivas
Abstract: Techniques to control flight of an aircraft are disclosed. In various embodiments, a set of inputs associated with a requested set of forces and moments to be applied to the aircraft is received. An optimal mix of actuators and associated actuator parameters to achieve to an extent practical the requested forces and moments is determined.
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公开(公告)号：US11034441B2
公开(公告)日：2021-06-15
申请号：US16441642
申请日：2019-06-14
Applicant: Wisk Aero LLC
Inventor： Zouhair Mahboubi , Gabe Hoffmann , Olivier Toupet , Herve Martins-Rivas
Abstract: Techniques to control flight of an aircraft are disclosed. In various embodiments, a set of inputs associated with a requested set of forces and moments to be applied to the aircraft is received. An optimal mix of actuators and associated actuator parameters to achieve to an extent practical the requested forces and moments is determined, including by minimizing a weighted set of costs that includes costs associated with one or more errors each corresponding to a difference between a requested force or moment and a corresponding force or moment achieved by the computed solution.
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Patent Agency Ranking
公开(公告)号：US11787535B2
公开(公告)日：2023-10-17
申请号：US17325629
申请日：2021-05-20
Applicant: Wisk Aero LLC
Inventor： Zouhair Mahboubi , Gabe Hoffmann , Olivier Toupet , Herve Martins-Rivas
CPC classification number: B64C29/00 , B64C27/28 , B64C29/0025 , G05D1/085 , G05D1/0808 , G05D1/101 , G05D1/102
Abstract: Techniques to control flight of an aircraft are disclosed. In various embodiments, a set of inputs associated with a requested set of forces and moments to be applied to the aircraft is received. An optimal mix of actuators and associated actuator parameters to achieve to an extent practical the requested forces and moments is determined.
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公开(公告)号：US20240002047A1
公开(公告)日：2024-01-04
申请号：US18467322
申请日：2023-09-14
Applicant: Wisk Aero LLC
Inventor： Zouhair Mahboubi , Gabe Hoffmann , Olivier Toupet , Herve Martins-Rivas
CPC classification number: B64C29/00 , G05D1/0808 , B64C27/28 , B64C29/0025 , G05D1/085 , G05D1/101 , G05D1/102
Abstract: Techniques to control flight of an aircraft are disclosed. In various embodiments, a set of inputs associated with a requested set of forces and moments to be applied to the aircraft is received. An optimal mix of actuators and associated actuator parameters to achieve to an extent practical the requested forces and moments is determined.
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公开(公告)号：US20210362847A1
公开(公告)日：2021-11-25
申请号：US17325629
申请日：2021-05-20
Applicant: Wisk Aero LLC
Inventor： Zouhair Mahboubi , Gabe Hoffmann , Olivier Toupet , Herve Martins-Rivas
Abstract: Techniques to control flight of an aircraft are disclosed. In various embodiments, a set of inputs associated with a requested set of forces and moments to be applied to the aircraft is received. An optimal mix of actuators and associated actuator parameters to achieve to an extent practical the requested forces and moments is determined.
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公开(公告)号：US12071231B2
公开(公告)日：2024-08-27
申请号：US18467322
申请日：2023-09-14
Applicant: Wisk Aero LLC
Inventor： Zouhair Mahboubi , Gabe Hoffmann , Olivier Toupet , Herve Martins-Rivas
CPC classification number: B64C29/00 , B64C27/28 , B64C29/0025 , G05D1/0808 , G05D1/085 , G05D1/101 , G05D1/102
Abstract: Techniques to control flight of an aircraft are disclosed. In various embodiments, a set of inputs associated with a requested set of forces and moments to be applied to the aircraft is received. An optimal mix of actuators and associated actuator parameters to achieve to an extent practical the requested forces and moments is determined.
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公开(公告)号：US10562620B2
公开(公告)日：2020-02-18
申请号：US15717716
申请日：2017-09-27
Applicant: WISK AERO LLC
Inventor： Ilan Kroo , Herve Martins-Rivas , Eric Allison
Abstract: In various embodiments, a tilt-wing aircraft includes a fuselage; a first wing tiltably mounted at or near a forward end of the fuselage; and a second wing rotatably mounted to the fuselage at a position aft of the first wing. A first plurality of rotors is mounted on the first wing at locations on or near a leading edge of the first wing, with two or more rotors being mounted on wing portions on each side of the fuselage; and a second plurality of rotors mounted on the second wing at locations on or near a leading edge of the second wing, with two or more rotors being mounted on wing portions on each side of the fuselage. A flight control system generates a set of actuators and associated actuator parameters to achieve desired forces and moments.
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