Helicopter autopilot

• US 20110022250A1
• Filed: 10/21/2008
• Published: 01/27/2011
• Est. Priority Date: 10/21/2008
• Status: Abandoned Application

• Current Assignee: Ron Wayne Hamburg
• Original Assignee: Ron Wayne Hamburg
• Inventors: Hamburg, Ron Wayne
• Application Number:
  US12/288,561
• Publication Number:
  US 20110022250A1
• Time in Patent Office: Days
• US Class Current: 701/11
• CPC Class Codes: G05D 1/102 specially adapted for vertical take-off of aircraft

Abstract

The Helicopter Autopilot operates by recording GPS (Global Positioning System) and/or accellerometer coordinates on CD-ROM during a programming flight or maneuver. To autopilot this flight plan, the received GPS coordinates that show the pilot'"'"'s real-time position, will be compared with the programmed GPS coordinates that represent the magnetic course high-lighted on the dashboard GPS terrain map display screen. The flight controls are computor adjusted until the helicopter is aligned with this pre-recorded magnetic course shown on the GPS display screen. The altitude, latitude, longitude and velocity are matched to these timed programmed coordinates. The automatic flight controls of the cyclic (main rotor tilt), the collective pitch (main rotor blades angle of attack), the anti-torque pedals (tail rotor blades angle of attack), and the throttle (engine power and RPM), which will change the yaw, pitch, roll and airspeed to again fly the helicopter through this pre-recorded GPS coordinate sequence.

Claims

1. The invention claimed is:

A Helicopter Autopilot system comprising of a GPS receiver, a magnetic compass, VOR, accellerometers, PCI atomic clock(s), four (4) to ten (10) microprocessors, four (4) servo motors or directly wired to existing motors, dashboard GPS display screen(s) functioning as an onboard computor that automatically adjusts the flight controls of the cyclic, collective pitch, anti-torque pedals and throttle to control yaw, pitch, roll and airspeed of the helicopter while flying through and matching real-time GPS coordinates to pre-recorded GPS coordinates that represent a magnetic course shown on the GPS display screen.

2. The invention claimed is:

A Helicopter Autopilot system and process comprising of autopiloting a helicopter using the procedure of flying a flight plan or maneuver and recording said GPS coordinates that the helicopter has flown through, as determined by the onboard GPS receiver and/or accellerometers and stored on CD-ROM at four (4) to (30) second intervals. The process is to include the recording of several flights on CD-ROM and then used in an autopilot system as described.)

3. The invention claimed is:

A Helicopter Autopilot system that utilizes a “

Standard Flight Plan Profile”

while autopiloting a helicopter to a GPS coordinate that has been input into the onboard computor data base and that identifies a landing location that is shown on the dashboard GPS terrain map display screen, this is depicted in FIG. 1 of the drawings.