Recovery system using vehicle state information

Patent metadata

Field	Value
Publication number	US-11208214-B2
Application number	US-202016744620-A
Country	US
Kind code	B2
Filing date	Jan 16, 2020
Priority date	Sep 9, 2019
Publication date	Dec 28, 2021
Grant date	Dec 28, 2021

Abstract

A selection is made between single stage and multistage parachute deployment for a vehicle based at least in part on vehicle state information. In the event multistage parachute deployment is selected, a drogue parachute is deployed during a first deployment stage and afterwards, a main parachute is deployed during a second deployment stage. In the event single stage parachute deployment is selected, at least the main parachute is deployed in a single stage where in the event the drogue parachute is deployed during the single stage, the drogue and main parachute are deployed simultaneously.

First claim

What is claimed is:

1. A system, comprising:
a recovery system controller which is configured to:
select between single stage parachute deployment and multistage parachute deployment for a vehicle based at least in part on vehicle state information;
in the event multistage parachute deployment is selected:
deploy a drogue parachute during a first deployment stage;
determine an amount of time to wait before deploying a main parachute in a second deployment stage based at least in part on vehicle state information; and
deploy the main parachute during a second deployment stage after the determined amount of time has elapsed; and

in the event single stage parachute deployment is selected, deploy at least the main parachute in a single stage.

2. The system recited in claim 1 , wherein at least one of the main parachute or the drogue parachute is deployed using one or more rockets.

3. The system recited in claim 1 , wherein selecting between single stage parachute deployment and multistage parachute deployment is based at least in part on airspeed.

4. The system recited in claim 1 , wherein selecting between single stage parachute deployment and multistage parachute deployment is based at least in part on a tilt angle associated with a tiltrotor included in the vehicle.

5. The system recited in claim 1 , wherein selecting between single stage parachute deployment and multistage parachute deployment includes comparing the vehicle state information against a threshold.

6. The system recited in claim 1 , wherein selecting between single stage parachute deployment and multistage parachute deployment is based at least in part on a state variable associated with the vehicle's mode of flight.

7. The system recited in claim 1 , wherein:
in the event multistage parachute deployment is selected, the recovery system controller is further configured to determine an amount of time between deployment of the drogue parachute and deployment of the main parachute based at least in part on the same vehicle state information that is used to select between single stage parachute deployment and multistage parachute deployment; and
the main parachute is deployed after the drogue parachute has deployed and the determined amount of time has elapsed.

8. The system recited in claim 1 , wherein:
in the event multistage parachute deployment is selected, the recovery system controller is further configured to determine an amount of time between deployment of the drogue parachute and deployment of the main parachute based at least in part on a second set of vehicle state information that is different from the vehicle state information that is used to select between single stage parachute deployment and multistage parachute deployment; and
the main parachute is deployed after the drogue parachute has deployed and the determined amount of time has elapsed.

9. The system recited in claim 1 , wherein:
in the event multistage parachute deployment is selected, the recovery system controller is further configured to determine an amount of time between deployment of the drogue parachute and deployment of the main parachute based at least in part on a second set of vehicle state information that is different from the vehicle state information that is used to select between single stage parachute deployment and multistage parachute deployment;
the main parachute is deployed after the drogue parachute has deployed and the determined amount of time has elapsed;
the vehicle state information that is used to select between single stage parachute deployment and multistage parachute deployment includes airspeed and excludes vehicle velocity direction; and
the second set of vehicle state information includes airspeed and vehicle velocity direction.

10. The system recited in claim 1 , wherein the recovery system controller is further configured to:
monitor three or more independent signals, each of which independently reports the vehicle state information; and
in the event a majority of the independent signals agree, save the vehicle state information from the majority of the independent signals that agree, wherein selecting between single stage parachute deployment and multistage parachute deployment includes using a most recently saved vehicle state information.

11. The system recited in claim 1 , wherein the recovery system controller is further configured to:
send a query to a flight controller and start a timer; and
in the event a reply is not received before the timer exceeds a timeout:
select between single stage parachute deployment and multistage parachute deployment;
in the event multistage parachute deployment is selected:
deploy the drogue parachute; and
after the drogue parachute has deployed, deploy the main parachute; and

in the event single stage parachute deployment is selected, deploy the main parachute without prior deployment of the drogue parachute.

12. The system recited in claim 1 , wherein the recovery system controller is further configured to:
send a query to a flight controller; and
in the event a reply indicates that the vehicle is not airworthy:
select between single stage parachute deployment and multistage parachute deployment;
in the event multistage parachute deployment is selected:
deploy the drogue parachute; and
after the drogue parachute has deployed, deploy the main parachute; and

in the event single stage parachute deployment is selected, deploy the main parachute without prior deployment of the drogue parachute.

13. A method, comprising:
selecting between single stage parachute deployment and multistage parachute deployment for a vehicle based at least in part on vehicle state information;
in the event multistage parachute deployment is selected:
deploying a drogue parachute during a first deployment stage;
determining an amount of time to wait before deploying a main parachute in a second deployment stage based at least in part on vehicle state information;
deploying the main parachute during a second deployment stage after the determined amount of time has elapsed; and

in the event single stage parachute deployment is selected, deploying at least the main parachute in a single stage.

14. The method recited in claim 13 , wherein at least one of the main parachute or the drogue parachute is deployed using one or more rockets.

15. The method recited in claim 13 , wherein selecting between single stage parachute deployment and multistage parachute deployment is based at least in part on airspeed.

16. The method recited in claim 13 , wherein selecting between single stage parachute deployment and multistage parachute deployment is based at least in part on a tilt angle associated with a tiltrotor included in the vehicle.

17. The method recited in claim 13 , wherein selecting between single stage parachute deployment and multistage parachute deployment includes comparing the vehicle state information against a threshold.

18. The method recited in claim 13 , wherein selecting between single stage parachute deployment and multistage parachute deployment is based at least in part on a state variable associated with the vehicle's mode of flight.

19. The method recited in claim 13 , wherein:
in the event multistage parachute deployment is selected, determining an amount of time between deployment of the drogue parachute and deployment of the main parachute based at least in part on the same vehicle state information that is used to select between single stage parachute deployment and multistage par

Assignees

• Kitty Hawk Corp

Inventors

• Western Craig
• Vander Lind Damon
• Miller Eric
• Yaru James Thomas
• Mattson Timothy
• Goessling Andrew David

Classifications

• B64C29/0033

  the propellers being tiltable relative to the fuselage · CPC title

• B64D17/80 Primary

  in association with aircraft, e.g. for braking thereof · CPC title

• B64D17/725

  by explosive means · CPC title

• B64D17/74 Primary

  Sequential deployment of a plurality of canopies · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title