IP Library › Granted Patent US 9,499,264
Granted Patent B2
US 9,499,264 · App. 14/725,567 · Granted Nov 22, 2016

Unmanned vehicle operating modes

Inventors: Thomas Zygmant (Southport, CT); Jesse J. Lesperance (Harvest, AL); Ira E. Zoock (Orange, CT); James A. Kelly (Middlebury, CT)
Assignee: SIKORSKY AIRCRAFT CORPORATION
B64C39/024G05D1/0055B64C2201/141
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,499,264
App. No.
14/725,567
Granted
Nov 22, 2016
Kind
B2
Abstract

An aircraft is provided and includes a frame, drive elements configured to drive movements of the frame and a computer configured to receive mission planning and manual commands and to control operations of the drive elements to operate in a safe mode in which mission commands are accepted but manual commands are refused, a manual mode in which mission commands are refused but manual commands are accepted and an enroute mode. The computer is further configured to only allow mode transitions between the safe and manual modes and between the safe and enroute modes.

Claims (17)

1. A vehicle, comprising:

a frame;

drive elements configured to drive movements of the frame; and

a computer, including at least a processor, configured to receive mission planning commands comprising at least one of mission details, on-board system details or waypoint setting and manual commands comprising local maneuvering commands and to control operations of the drive elements to operate in a safe mode in which the mission planning commands are accepted but the manual commands are refused, a manual mode in which the mission planning commands are refused but the manual commands are accepted and an enroute mode,

wherein the safe mode comprises a stationary mode characterized in that the frame is stationary relative to ground,

wherein the manual mode comprises a movable mode characterized in that the frame is movable relative to the ground, and

wherein the computer is further configured to only allow mode transitions directly between the safe and manual modes and directly between the safe and enroute modes.

2. The vehicle according to claim 1 , wherein the frame is manned and crewed or un-crewed or unmanned.

3. The vehicle according to claim 1 , wherein the computer executes the mission planning commands during the enroute mode.

4. The vehicle according to claim 1 , wherein the computer is receptive of a stop command, which initiates a transition from the manual mode to the safe mode and from the enroute mode to the safe mode.

5. A vehicle, comprising:

a frame;

drive elements configured to drive movements of the frame; and

a computer, including at least a processor, configured to receive mission planning commands comprising at least one of mission details, on-board system details or waypoint setting and manual commands comprising local maneuvering commands and to control operations of the drive elements to operate in a ground stationary mode in which the mission planning commands are accepted but the manual commands are refused, in a hover stationary mode in which the mission planning commands are accepted but the manual commands are refused, a ground manual mode in which the mission planning commands are refused but the manual commands and a first stop command are accepted, a hover manual mode in which the mission planning commands are refused but the manual commands and a second stop command are accepted and an enroute mode in which the mission planning commands are executed and a third stop command is accepted,

wherein the safe mode comprises a stationary mode characterized in that the frame is stationary relative to ground,

wherein the manual mode comprises a movable mode characterized in that the frame is movable relative to the ground, and

wherein the computer is further configured to only allow mode transitions directly between the ground manual mode and the ground stationary mode upon receipt of the first stop command, directly between the ground stationary mode and the hover stationary mode, directly between the hover manual mode and the hover stationary mode upon receipt of the second stop command and directly between the enroute mode and the hover stationary mode upon receipt of the third stop command.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 29, 2015
From: ZYGMANT, THOMAS; LESPERANCE, JESSE J.; ZOOCK, IRA E.; KELLY, JAMES A.
To: SIKORSKY AIRCRAFT CORPORATION
Reel/Frame 035744/0814 →
Continuity (2)
Provisional Application 62005460 · May 30, 2014
Related Publication 20150346725A1 · Dec 3, 2015