Predicted path selection system and method for hazard coding in selectively constrained aircraft control systems

• US 8,065,043 B2
• Filed: 06/10/2010
• Issued: 11/22/2011
• Est. Priority Date: 02/28/2006
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Gremmert, Scott R.
• Primary Examiner(s): Hellner; Mark
• Assistant Examiner(s): Algahaim; Helal A
• Application Number:
  US12/813,238
• Publication Number:
  US 20100250032A1
• Time in Patent Office: 530 Days
• Field of Search: 701/3, 701/9, 701/14, 701/120, 701/207, 701/209, 701/301
• US Class Current: 701/9
• CPC Class Codes: G05D 1/101 specially adapted for aircraft

Abstract

A surveillance system detects potential hazards and alerts the pilot to them. The alerts can be modified to indicate proximity to the predicted path of the aircraft. An autopilot receives instructions from a flight management system (FMS) regarding a planned path and is subject to constraints preempting the planned path. The surveillance system selects which of the planned and a constrained path will be followed for alerting and hazard coding purposes. Means are disclosed to determine when the constrained path will be followed by comparing the current position of an aircraft, the planned path, and the constraint data. Current positions exceeding the tolerance cause the surveillance system to select the planned path as the future path to be followed. If initiation of a constraint has been detected and the current position is within the tolerance, the surveillance system selects the constrained path as the future path.

Claims

1. A method for selecting a predicted path, the method comprising:

detecting activation of a constraint at a surveillance system;

imposing the constraint on an aircraft flight controller;

detecting the imposition of the constraint by means of a surveillance means;

detecting hazard locations;

calculating a planned flight path;

detecting an aircraft current location;

comparing the aircraft current location to the constraint to determine a variation of aircraft current location from the constraint;

providing alerts of hazards located along the planned path if an absolute value of a difference between an aircraft current altitude and the constraint is greater than the tolerance; and

refraining from providing alerts of hazards located along the planned path if the absolute value is less than the tolerance.

2. The method of claim 1, further comprising refraining from transmitting an indication of deactivation of the constraint to the surveillance means.

3. The method of claim 2, wherein providing alerts comprises visually displaying relevant symbols representing hazards.

4. The method of claim 3, wherein refraining from providing alerts comprises visually displaying non-relevant symbols representing hazards.

5. The method of claim 4, wherein relevant symbols and non-relevant symbols are distinguished by at least one visual attribute.

6. The method of claim 3 wherein visually displaying relevant symbols further comprises displaying relevant symbols in a navigational display.

7. The method of claim 1, wherein the constraint is an altitude constraint.

8. The method of claim 1, wherein calculating a planned flight path comprises repeatedly updating the planned flight path according to the aircraft current location.

9. A system for selecting a predicted path, the system comprising:

a flight controller controlling actuators coupled to control surfaces and the propulsion systems of an aircraft and configured to cause the aircraft to follow an actual path, the flight controller receiving a first input describing a planned path and a second input indicating a constraint on the actual path in at least one direction, the flight controller configured to selectively cause the aircraft to conform the actual path to the planned path or a constrained path corresponding to the constraint;

a flight planner configured to calculate a planned path and input the planned path to the flight controller;

a surveillance system configured to detect locations of hazards and produce a symbolic display comprising relevant symbols corresponding to hazards near a predicted flight path and non-relevant symbols corresponding to hazards away from the predicted flight path, the surveillance system being further configured to detect activation of the constraint and to compare a current aircraft location to the constrained path upon detecting activation of the constraint, and displaying hazards located along the planned path as relevant when the aircraft location is beyond a tolerance distance from the constrained path.

10. The system of claim 9, wherein the surveillance system displays hazards near the constrained path as relevant when the aircraft location is within the tolerance distance from the constrained path.

11. The system of claim 9, wherein the surveillance system displays hazards near a tactical path as relevant when the aircraft is not within the tolerance distance of the constrained path or the planned path, the tactical path corresponding to a current trajectory of the aircraft.

12. The system of claim 9, wherein the planning means calculates an updated path directing the aircraft from the aircraft location to the planned path.

13. The system of claim 9, wherein the flight planner is configured to calculate a planned path comprising a plurality of interconnected waypoints and to designate one of the plurality of waypoints corresponding to the aircraft current position as a from point, the flight planner receiving the activation output and inputting the from point to the surveillance system as a constraint waypoint if the flight controller is conforming to the constrained path.