OMEGA-VOR/DME positional data computer for aircraft

• US 3,941,983 A
• Filed: 01/27/1975
• Issued: 03/02/1976
• Est. Priority Date: 01/27/1975
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Sperry Rand Corporation
• Inventors: Baker, Donald H.
• Primary Examiner(s): Morrison, Malcolm A.
• Assistant Examiner(s): Smith, Jerry
• Application Number:
  US05/544,105
• Time in Patent Office: 400 Days
• Field of Search: 235/150.2, 235/150.26, 235/150.27, 235/150.272, 343/103, 343/105 R, 343/112 R, 343/112 C
• US Class Current: 701/218
• CPC Class Codes: G06G 7/78 for direction-finding, locating, distance or velocity measuring, or navigation systems

Abstract

Apparatus for combining positional data from OMEGA and VOR/DME radio navigation systems to provide computed positional data corresponding thereto includes a circuit for generating an OMEGA compensation in accordance with the difference between the computed value of the positional data and the VOR/DME value thereof. The computed value is provided by algebraically adding the OMEGA compensation to the positional data from the OMEGA system. The gain of the OMEGA compensation circuit is adjusted in an inverse relation with respect to the range of the aircraft from the VOR/DME station thus providing high accuracy positional data throughout the enroute flight of the aircraft without the attendant complexities and inaccuracies normally associated with the separate OMEGA and VOR/DME radio navigation aids.

Claims

1. A computer for use in aircraft for providing a computed positional data signal in response to an OMEGA positional data signal from an OMEGA system, a VOR/DME positional data signal from VOR/DME apparatus tuned to a stationary VOR/DME facility and a range signal representative of the distance of said aircraft from said VOR/DME facility, comprising:

first summing means responsive to said VOR/DME positional data signal and said computed positional data signal for providing a positional data error signal representative of the difference therebetween,

Omega compensation means responsive to said positional data error signal and said range signal for providing an OMEGA compensation signal with a dependance on said positional data error signal in accordance with an inverse function of said distance, and

second summing means responsive to said OMEGA positional data signal and said OMEGA compensation signal for providing said computed positional data signal in accordance with the algebraic sum thereof.

2. The computer of claim 1 in which said OMEGA compensation means comprises:

gain adjusting means responsive to said positional data error signal and said range signal for providing said positional data error signal at a gain adjusted in accordance with said inverse function of said distance, and

integrator means coupled to said gain adjusting means for providing said OMEGA compensation signal in accordance with the integral of said gain adjusted positional data error signal.

3. The computer of claim 2 further including means for clamping said integrator in response to a signal indicative of invalidity of said VOR/DME positional data signal.

4. The computer of claim 2 further including means for obtaining said computed positional data signal directly from said VOR/DME positional data signal in response to a signal indicative of invalidity of said OMEGA positional data signal.

5. A computer for use in aircraft for providing a computed positional data signal in response to an OMEGA positional data signal from an OMEGA system, a VOR/DME positional data signal from VOR/DME apparatus tuned to a stationary VOR/DME facility and a range signal representative of the distance of said aircraft from said VOR/DME facility, comprising:

means for storing a previous value of an OMEGA compensation signal,

first means for adding the current value of said OMEGA positional data signal to said previous value of said OMEGA compensation signal to provide a temporary computed positional data signal,

second means for subtracting the value of said temporary computed positional data signal from the current value of said VOR/DME positional data signal to provide a positional data error signal,

third means for computing a gain value in accordance with an inverse function of said distance,

fourth means for multiplying the value of said positional data error signal by said gain value to provide an intergrand value,

fifth means for multiplying said intergrand value by the time elapsed since the computation for said previous value of said OMEGA compensation signal and for adding the result to said previous value of said OMEGA compensation signal to provide an updated value of said OMEGA compensation signal, thereby performing a time integration of said positional data error signal at a gain determined by said third means, and

sixth means for adding said updated value of said OMEGA compensation signal to said current value of said OMEGA positional data signal to provide said computed positional data signal.