Navigation mode selection apparatus

• US 4,806,940 A
• Filed: 04/30/1986
• Issued: 02/21/1989
• Est. Priority Date: 04/30/1986
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Reed, Michael D., Harral, Blake G.
• Primary Examiner(s): Blum, Theodore M.
• Assistant Examiner(s): Issing, Gregory C.
• Application Number:
  US06/858,410
• Time in Patent Office: 1,028 Days
• Field of Search: 364/164, 364/451, 364/449, 342/457, 342/451, 342/410-413, 455/133-135, 340/517, 340/521
• US Class Current: 342/451
• CPC Class Codes: G01C 21/005 with correlation of navigation data from several sources, e.g. map or contour matching G01C21/30 takes precedence
• CPC Class Codes: G01C 21/165 combined with non-inertial navigation instruments
• CPC Class Codes: G01C 21/188 for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems
• CPC Class Codes: G01S 5/02 using radio waves using satellite radio beacon systems for determining position G01S19/00

Abstract

An aircraft navigation system supporting a plurality of navigation modes. An error estimator for each navigation mode provides an estimated navmode error signal representative of an estimate of the error in the position signal generated by the associated navmode. A navigation mode selector enables the navmode having the smallest estimated navmode error signal that is consistent with procedure specified navaid criteria. The navmode computed position signal is processed through a low pass position filter. The estimated navmode error signal associated with the selected navmode is processed through a low pass position error filter having the same time constant as the low pass position filter to provide an estimated position error. The estimated position error is utilized in providing the INS and DEAD RECKONING navigation as well as to set a threshold for estimated navmode error signals sensor data validation.

Claims

1. A navigation mode selection apparatus for utilization in a navigation system of the type having a plurality of navigation modes, each mode providing a position signal generated by a respective one of a plurality of navigation mode position determining procedures, comprising:

error estimator means for providing mode error signals representative of position error estimates for each of said plurality of navigation modes; and

navigation mode selector means responsive to said mode error signals for selecting from said plurality of navigation modes one navigation mode having a mode error signal representative of a position error estimate which is less than position error estimates represented by mode error signals from other navigation modes of said plurality of navigation modes and for providing said mode error signal of said one navigation mode;

low pass position filter means having a predetermined time constant and coupled to receive said position signal for providing said position signal with a slow-in function, thereby eliminating abrupt position signal changes when switching between navigation modes;

low pass position error filter means having a time constant equal to said predetermined time constant and coupled to receive said mode error signals of said one navigation mode from said navigation mode selector means for providing a position error signal representative of estimated position error to said one navigation mode; and

validation means coupled to said low pass position filter means and said low pass position error filter means for validating input navigation data presented by said one navigation mode by comparing said position signal to a threshold set in accordance with said position error signal, whereby an unfavorable comparison of said position signal to said threshold causes said navigation mode selector means to select a navigation mode other than said one navigation mode.

2. The apparatus of claim 1 wherein said navigation mode selector means comprises means responsive to criteria signals representative of a predetermined procedure specified criteria for selecting said one navigation mode consistent with criteria represented by said criteria signals.

3. The apparatus of claim 1 in which said validation means comprises means for determining a difference between said position signal and said position error signal and for comparing said difference to said threshold.

4. The apparatus of claim 2 wherein:

said plurality of navigation modes includes an INS navigation mode associated with an inertial navigation system,

said error estimator means includes an INS error estimator for providing an estimated INS navigation mode error signal,

said INS error estimator being responsive to said position error signal for providing said estimated INS navigation mode error signal as a function thereof, and said INS navigation mode includes means for correcting said position signal generated by said INS navigation mode in accordance with said estimated INS navigation mode error signal.

5. The apparatus of claim 2 in which

said plurality of navigation modes includes a DEAD RECKONING navigation mode associated with a DEAD RECKONING procedure apparatus in said navigation system,

said error estimator means includes a DEAD RECKONING error estimator for providing an estimated DEAD RECKONING navigation mode error signal,

said DEAD RECKONING error estimator being responsive to said estimated position error signal for providing said estimated DEAD RECKONING navigation mode error signal as a function thereof, and

said DEAD RECKONING navigation mode includes means for correcting said position signal generated thereby in accordance with said estimated DEAD RECKONING navigation mode error signal.