Touchdown control system

Patent metadata

Field	Value
Publication number	US-10315780-B2
Application number	US-201715496126-A
Country	US
Kind code	B2
Filing date	Apr 25, 2017
Priority date	Apr 25, 2017
Publication date	Jun 11, 2019
Grant date	Jun 11, 2019

Abstract

A touchdown control system for a vertical take-off and landing (VTOL) aircraft including a detection controller receptive to aircraft state signals including one or more of an altitude signal, an aircraft attitude signal, an external environment signal, an aircraft velocity signal, an attitude rate signal, and a proximity signal. An enable controller is operatively connected to the detection controller. The enable controller selectively provides a touchdown control signal based on one or more of the altitude signal, the aircraft attitude signal, the external environment signal, the aircraft velocity signal, the attitude rate signal, and the proximity signal. A regulation controller is operatively connected to the enable controller. The regulation controller selectively adjusts aircraft control surfaces based on the touchdown control signal to facilitate final touchdown of the VTOL aircraft.

First claim

What is claimed is:

1. A touchdown control system for a vertical take-off and landing (VTOL) aircraft comprising:
a detection controller receptive to aircraft state signals including one or more of an altitude signal, an aircraft attitude signal, an external environment signal, an aircraft velocity signal, an attitude rate signal, and a proximity signal;
an enable controller operatively connected to the detection controller, the enable controller selectively providing a touchdown control signal based on one or more of the altitude signal, the aircraft attitude signal, the external environment signal, the aircraft velocity signal, the attitude rate signal, and the proximity signal, wherein the enable controller issues the touchdown control signal based on an operating mode of the VTOL aircraft; and
a regulation controller operatively connected to the enable controller, the regulation controller selectively adjusting aircraft control surfaces based on the touchdown control signal to facilitate final touchdown of the VTOL aircraft.

2. The touchdown control system according to claim 1 , wherein the detection controller determines a proximity of a landing surface and an undesirable aircraft condition based on signals from the one or more of the altitude signal, the aircraft attitude signal, the external environment signal, the aircraft velocity signal, the attitude rate signal, and the proximity signal.

3. The touchdown control system according to claim 2 , wherein the undesirable aircraft condition includes one or more of an aircraft attitude exceeding a pre-selected aircraft attitude threshold, aircraft velocity exceeding a pre-selected velocity threshold, aircraft attitude exceeding a pre-selected attitude threshold, wind exceeding a pre-selected wind speed threshold, and an attitude of a landing surface exceeding a pre-selected landing surface attitude threshold.

4. The touchdown control system according to claim 2 , wherein the undesirable aircraft condition includes at least of a one engine inoperative (OEI) condition, a multiple engine inoperative (MEI) condition, and an all engine inoperative (AEI) condition.

5. The touchdown control system according to claim 1 , wherein the regulation controller selectively controls one or more of a yaw command, a pitch command, a roll command, a lift command, a velocity command, an attitude command, and a thrust command of the VTOL aircraft based on the touchdown control signal from the enable controller.

6. A vertical take-off and landing (VTOL) aircraft comprising:
an airframe;
a main rotor assembly supported by the airframe;
at least one engine operatively connected to the main rotor assembly;
a plurality of aircraft control surfaces associated with at least one of the main rotor assembly and the airframe; and
a touchdown control system for a vertical take-off and landing (VTOL) aircraft comprising:
a detection controller receptive to aircraft state signals including one or more of an altitude signal, an aircraft attitude signal, an external environment signal, a velocity signal, an attitude rate signal, and a proximity signal;
an enable controller operatively connected to the detection controller, the enable controller selectively providing a touchdown control signal based on one or more of the altitude signal, the aircraft attitude signal, the external environment signal, the velocity signal, the attitude rate signal, and the proximity signal, wherein the enable controller issues the touchdown control signal based on an operating mode of the VTOL aircraft; and
a regulation controller operatively connected to the enable controller and one or more of the plurality of aircraft control surfaces, the regulation controller selectively adjusting aircraft control surfaces based on the touchdown control signal to facilitate final touchdown of the VTOL aircraft.

7. The VTOL aircraft according to claim 6 , wherein the detection controller determines a proximity of a landing surface and an undesirable aircraft condition based on signals from the one or more of the altitude signal, the aircraft attitude signal, the external environment signal, the aircraft velocity signal, the aircraft attitude signal, and the proximity signal.

8. The VTOL aircraft according to claim 7 , wherein the undesirable aircraft condition includes one or more of an aircraft attitude exceeding a pre-selected aircraft attitude threshold, aircraft velocity exceeding a pre-selected velocity threshold, aircraft attitude exceeding a pre-selected attitude threshold, wind exceeding a pre-selected wind speed threshold, and an attitude of a landing surface exceeding a pre-selected landing surface attitude threshold.

9. The VTOL aircraft according to claim 7 , wherein the at least one engine includes multiple engines, the undesirable aircraft condition including a malfunction of one or more of the multiple engines generating at least one of a one engine inoperative (OEI) condition, a multiple engine inoperative (MEI) condition, and an all engine inoperative (AEI) condition.

10. The VTOL aircraft according to claim 6 , wherein the regulation controller selectively controls one or more of a yaw command, a pitch command, a roll command, a lift command, an aircraft velocity command, an aircraft attitude command, and a thrust command of the VTOL aircraft based on the touchdown control signal from the enable controller.

11. The VTOL aircraft according to claim 6 , wherein the airframe includes an extending tail, and a tail rotor assembly supported by the extending tail.

12. The VTOL aircraft according to claim 11 , wherein the tail rotor assembly comprises a pusher-prop.

13. A method of controlling a vertical take-off and landing aircraft during touchdown comprising:
detecting, through a processor, an imminent touchdown of the VTOL aircraft;
sensing through the processor, a condition of the VTOL aircraft, including one of an pre-selected aircraft condition, a selected ground based condition, a selected wind speed, a selected aircraft velocity, and a type of passenger in the VTOL aircraft;
enabling, through the processor, computer control of one or more aircraft control surfaces based on the condition of the VTOL aircraft; and
regulating, through the processor, control of the one or more aircraft control surfaces based on the condition of the VTOL aircraft to facilitate touchdown.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Waltner Peter J
• Macko Nikolas A
• Bazzani Daniel

Classifications

• B64D45/06 Primary

  mechanical · CPC title

• B64C2027/8236

  including pusher propellers · CPC title

• B64C27/82

  characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft · CPC title

• B64C27/10 Primary

  arranged coaxially · CPC title

• G05D1/0858

  specially adapted for vertical take-off of aircraft · CPC title