Tactile and peripheral vision combined modality hover drift cueing

• US 10,392,124 B2
• Filed: 06/29/2016
• Issued: 08/27/2019
• Est. Priority Date: 03/26/2014
• Status: Active Grant

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Colby, Steven D.
• Primary Examiner(s): Elchanti, Hussein
• Application Number:
  US15/196,367
• Publication Number:
  US 20170096237A1
• Time in Patent Office: 1,154 Days
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: G06F 3/011 Arrangements for interaction with the human body, e.g. for user immersion in virtual reality blind teaching G09B21/00
• CPC Class Codes: G06F 3/016 Input arrangements with force or tactile feedback as computer generated output to the user

Abstract

Combined modality hover drift cueing methods, systems and computer readable media are disclosed. For example, some implementations can include a system comprising one or more sensors, and a combined modality hover drift cueing controller coupled to the one or more sensors and configured to determine hover drift and to control a plurality of indicators in response to determined hover drift. The system can also include a mode selector coupled to the combined modality hover drift cueing controller and configured to provide an indication of mode selection between one of a first mode, a second mode and a third mode, wherein the first mode is a combined modality mode. The system can further include a peripheral vision hover drift indicator coupled to the controller and mounted on an inside surface of an aircraft cockpit, and a tactile feedback indicator coupled to the controller.

Claims

1. A method comprising:

receiving, at a processor, vehicle position information from one or more sensors disposed on a vehicle;

determining, at the processor, position drift based on the received vehicle position information;

determining, at the processor, if a combined mode is selected, wherein, if the combined mode is selected, a cueing signal is transmitted to both a peripheral vision position drift indicator and a tactile feedback indicator; and

if the combined mode is not selected, determining if a peripheral only mode is selected, wherein if peripheral only mode is selected, the cueing signal is transmitted to the peripheral vision position drift indicator; and

if the peripheral only mode is not selected, transmitting the cueing signal to the tactile feedback indicator; and

controlling, with the processor, at least one of the peripheral vision position drift indicator and the tactile feedback indicator based on the combined mode and peripheral only mode, the tactile feedback indicator being configured to indicate the position drift by generating tactile feedback, and the peripheral vision position drift indicator and the tactile feedback indicator being onboard the vehicle.

2. The method of claim 1, wherein the vehicle includes one of a land vehicle, a surface water vessel, an underwater vessel, an aircraft and a spacecraft.

3. The method of claim 1, wherein the peripheral vision position drift indicator includes a first position drift indicator and a second position drift indicator.

4. The method of claim 3, wherein the peripheral vision position drift indicator further comprises a third position drift indicator coupled to the processor.

5. The method of claim 3, wherein the first position drift indicator is configured to indicate fore/aft drift.

6. The method of claim 5, wherein the second position drift indicator is configured to indicate lateral drift.

7. The method of claim 5, wherein the first position drift indicator is mounted on a door frame of the vehicle adjacent an operator seat so as to be visible in a peripheral vision field of an operator when the operator is positioned in the operator seat.

8. The method of claim 6, wherein the second position drift indicator is mounted adjacent to a central instrument panel of the vehicle so as to be visible in a peripheral vision field of an operator when the operator is positioned in an operator seat of the vehicle.

9. A nontransitory computer readable medium having stored thereon software instructions that, when executed, cause a processor to perform operations comprising:

receiving, at a processor, aircraft position information from one or more sensors disposed on an aircraft;

determining, at the processor, hover drift based on the received aircraft position information;

determining, at the processor, if a combined mode is selected, wherein, if the combined mode is selected, a cueing signal is transmitted to both a peripheral vision hover drift indicator and a tactile feedback indicator;

if the combined mode is not selected, determining if a peripheral only mode is selected, wherein if peripheral only mode is selected, the cueing signal is transmitted to the peripheral vision hover drift indicator;

if the peripheral only mode is not selected, transmitting the cueing signal to the tactile feedback indicator; and

controlling, with the processor, at least one of the peripheral vision hover drift indicator and the tactile feedback indicator based on the combined mode and the peripheral only mode, the tactile feedback indicator being configured to indicate the hover drift by generating tactile feedback, and the peripheral vision hover drift indicator and the tactile feedback indicator being onboard the vehicle.

10. The nontransitory computer readable medium of claim 9, wherein the one or more sensors include one or more of a radar altimeter, an air data system, an inertial navigation system, a traffic alert and collision avoidance system, an Enhanced Ground Proximity Warning System (EGPWS)/Controlled Flight Into Terrain (CFIT) system, a digital map, a terrain database, a Global Positioning System (GPS) receiver, a Differential Global Positioning System (DGPS) receiver, a microwave radar, a forward looking infrared (FLIR) camera, and/or a video camera.

11. The nontransitory computer readable medium of claim 9, wherein the peripheral vision hover drift indicator includes a first hover drift indicator and a second hover drift indicator.

12. The nontransitory computer readable medium of claim 11, wherein the first hover drift indicator is configured to indicate fore/aft drift and is mounted on a door frame of the aircraft adjacent to a pilot seat so as to be visible in a peripheral vision field of a pilot when the pilot is positioned in the pilot seat.

13. The nontransitory computer readable medium of claim 11, wherein the second hover drift indicator is configured to indicate lateral drift and is mounted adjacent to a central instrument panel of the aircraft so as to be visible in a peripheral vision field of a pilot when the pilot is positioned in a pilot seat of the aircraft.