Helicopter integrated fire and flight control having coordinated area bombing control

• US 5,310,135 A
• Filed: 10/28/1992
• Issued: 05/10/1994
• Est. Priority Date: 10/28/1992
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Lappos, Nicholas D., Fowler, Donald W.
• Primary Examiner(s): Focarino, Margaret A.
• Assistant Examiner(s): Ellis, Christopher P.
• Application Number:
  US07/967,308
• Time in Patent Office: 559 Days
• Field of Search: 244/17.13, 244/75 R, 244/76 R, 244/221, 244/190, 244/137.4, 89/41.21, 364/423, 364/424.01, 364/434
• US Class Current: 244/17.13
• CPC Class Codes: B64C 13/50 using electrical energy
• CPC Class Codes: F41G 3/22 for vehicle-borne armament, e.g. on aircraft
• CPC Class Codes: F41G 5/18 Tracking systems for guns on aircraft
• CPC Class Codes: F41G 9/002 for guiding a craft to a correct firing position for bombing control F41G9/02
• CPC Class Codes: G05D 1/0858 specially adapted for vertical take-off of aircraft

Abstract

During operation of a flight control system in a coordinated area bombing mode, one pair in a group of pairs of fire control azimuth coordinate error signal and elevation coordinate error signals are faded-in as the aircraft yaw attitude reference and pitch attitude reference, respectively. Each pair is respectively indicative of the change in aircraft yaw attitude and pitch attitude for an aircraft reference axis to be aligned with an aiming line of sight. The aiming line of sight corresponds to a target location within a selected target area. A firing signal is provided in response to both the azimuth and elevation coordinate error signals being below respective threshold magnitudes, and the next pair in the group of pairs of azimuth and elevation coordinate error signals provide the aircraft attitude reference. A selected weapon is fired in response to the firing signal.

Claims

1. An aircraft flight control system for providing control surface command signals to the aircraft control surfaces thereby controlling the yaw, pitch, roll and lift attitude axes of the aircraft in flight, comprising:

fire control means for providing at least one pair of azimuth and elevation coordinate error signals, said pairs of azimuth and elevation coordinate error signals each being indicative of the change in aircraft yaw attitude and pitch attitude for an aircraft to be aligned with an aiming attitude;

means for providing a coordinated area bombing signal in response to activation of a flight control system coordinated area bombing mode; and

one of said pairs of azimuth and elevation coordinate error signals providing the aircraft yaw attitude reference and pitch attitude reference in response to said coordinated area bombing signal.

2. An aircraft flight control system according to claim 1 further comprising:

means for providing a firing signal in response to both said azimuth and elevation coordinate error signals in said one of said pairs of azimuth and elevation coordinate error signals being below respective threshold magnitudes; and

weapons control means responsive to said firing signal for firing a weapon.

3. An aircraft flight control system according to claim 2 further comprising means responsive to said firing signal for selecting the next pair of azimuth and elevation coordinate error signals as the aircraft yaw and pitch attitude reference.

4. An aircraft flight control system according to claim 1 further comprising:

means for providing a pattern shape signal indicative of the shape of a target area;

means for providing a pattern azimuth signal indicative of the orientation of said target area;

means for providing a pattern size signal indicative of the size of said target area;

means for providing a weapons signal indicative of the number of weapon rounds to be fired into said target area; and

means responsive to said pattern shape signal, said pattern azimuth signal, said pattern size signal and said weapons signal for providing target coordinate signals each being indicative of a target location within said target area corresponding to each of said weapon rounds, each of said target locations being determined with respect to a target area reference point.

5. An aircraft flight control system according to claim 4 further comprising:

target tracking means for providing a target azimuth signal and a target elevation signal indicative of the azimuth and elevation of said target area reference point with respect to an aircraft reference axis;

means for providing a range signal indicative of the range from said aircraft to said target area reference point;

means for providing a yaw attitude signal indicative of the aircraft yaw attitude;

means for providing a pitch attitude signal indicative of the aircraft pitch attitude; and

signal processing means responsive to said target azimuth signal, said target elevation signal, said range signal, said target coordinate signals, said yaw attitude signal and said pitch attitude signal for providing said pairs of elevation and azimuth coordinate error signals, each pair of said elevation and azimuth coordinate error signals corresponding to one of said target locations within said target area.

6. An aircraft flight control system according to claim 4 further comprising a pilot interface operable by a pilot for providing said pattern shape signal, said pattern azimuth signal, said pattern size signal and said weapons signal.

7. An aircraft flight control system according to claim 5 further comprising:

weapon indicating means for providing a weapon indication signal indicative of the type of weapons selected for firing at said target locations;

means responsive to said weapon indicating signal for providing bore sight correction signals each indicative of the bore sight offset between one of said selected weapons and said aircraft reference axis;

means responsive to said weapon indicating signal, said target azimuth signal, said target elevation signal and said range signal for providing weapon trajectory signals each indicative of the change in aircraft attitude required for a weapon to strike a corresponding target location due to weapon trajectory; and

said signal processing means being further responsive to said bore sight correction signals and said weapon trajectory signals for providing said pairs of azimuth and elevation coordinate error signals.

8. An aircraft flight control system according to claim 1 further comprising switch means operable by a pilot, said means for providing a coordinated area bombing signal being responsive to the continuous activation of said switch means for providing said programmed area bombing signal, said means for providing a coordinated area bombing signal being responsive to the deactivation of said switch means for removing said coordinated area bombing signal.

9. A helicopter integrated fire and flight control system for providing control surface command signals to the helicopter control surfaces thereby controlling the yaw, pitch, roll and lift attitude axes of the helicopter in flight, comprising:

fire control means for providing at least one pair of azimuth and elevation coordinate error signals, said pairs of azimuth and elevation coordinate error signals each being indicative of the change in aircraft yaw attitude and pitch attitude for an aircraft to be aligned with an aiming attitude;

means for providing a coordinated area bombing signal in response to activation of a flight control system coordinated area bombing mode;

one of said pairs of azimuth and elevation coordinate error signals providing the aircraft yaw attitude reference and pitch attitude reference in response to said coordinated area bombing signal;

means for providing a firing signal in response to both said azimuth and elevation coordinate error signals in said one of said pairs of azimuth and elevation coordinate error signals being below respective threshold magnitudes; and

weapons control means responsive to said firing signal for firing a weapon.

10. A helicopter integrated fire and flight control system according to claim 9 further comprising means responsive to said firing signal for selecting the next pair of azimuth and elevation coordinate error signals as the aircraft yaw and pitch attitude reference.

11. A helicopter integrated fire and flight control system according to claim 10 further comprising:

means for providing a pattern shape signal indicative of the shape of a target area;

means for providing a pattern azimuth signal indicative of the orientation of said target area;

means for providing a pattern size signal indicative of the size of said target area;

means for providing a weapons signal indicative of the number of weapon rounds to be fired into said target area; and

means responsive to said pattern shape signal, said pattern azimuth signal, said pattern size signal and said weapons signal for providing target coordinate signals each being indicative of a target location within said target area corresponding to each of said weapon rounds, each of said target location being determined with respect to a target area reference point.

12. A helicopter integrated fire and flight control system according to claim 11 further comprising:

target tracking means for providing a target azimuth signal and a target elevation signal indicative of the azimuth and elevation of said target area reference point with respect to an aircraft reference axis;

means for providing a range signal indicative of the range from said aircraft to said target area reference point;

means for providing a yaw attitude signal indicative of the aircraft yaw attitude;

means for providing a pitch attitude signal indicative of the aircraft pitch attitude; and

signal processing means responsive to said target azimuth signal, said target elevation signal, said range signal, said target coordinate signals, said yaw attitude signal and said pitch attitude signal for providing said pairs of elevation and azimuth coordinate error signals, each pair of said elevation and azimuth coordinate error signals corresponding to one of said target locations within said target area.

13. A helicopter integrated fire and flight control system according to claim 12 further comprising a pilot interface operable by a pilot for providing said-pattern shape signal, said pattern azimuth signal, said pattern size signal and said weapons signal.

14. A helicopter integrated fire and flight control system according to claim 12 further comprising:

weapon indicating means for providing a weapon indication signal indicative of the type of weapons selected for firing at said target locations;

means responsive to said weapon indicating signal for providing bore sight correction signals each indicative of the bore sight offset between one of said selected weapons and said aircraft reference axis;

means responsive to said weapon indicating signal, said target azimuth signal, said target elevation signal and said range signal for providing weapon trajectory signals each indicative of the change in aircraft attitude required for a weapon to strike a corresponding target location due to weapon trajectory; and

said signal processing means being further responsive to said bore sight correction signals and said weapon trajectory signals for providing said pairs of azimuth and elevation coordinate error signals.

15. A helicopter integrated fire and flight control system according to claim 9 further comprising switch means operable by a pilot, said means for providing a coordinated area bombing signal being responsive to the continuous activation of said switch means for providing said programmed area bombing signal, said means for providing a coordinated area bombing signal being responsive to the deactivation of said switch means for removing said coordinated area bombing signal.