Intervention flight management system

• US 4,811,230 A
• Filed: 08/15/1986
• Issued: 03/07/1989
• Est. Priority Date: 08/15/1986
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Edmonds, Thomas E., Graham, Donald A.
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): Black, Thomas G.
• Application Number:
  US06/897,141
• Time in Patent Office: 935 Days
• Field of Search: 364/424, 364/427, 364/428, 364/436, 364/430, 364/439, 364/433, 364/442, 364/443, 73/178 T
• US Class Current: 701/16
• CPC Class Codes: G05D 1/0061 for transition from automatic pilot to manual pilot and vice versa
• CPC Class Codes: G05D 1/0607 specially adapted for aircraft

Abstract

An Intervention Flight Management System (IFMS) that allows a pilot to intervene in the operation of a preprogrammed flight management computer and change the speed and/or flight path of an airplane in response to air traffic control (ATC) instructions is disclosed. The IFMS includes an IFMS control panel via which the pilot interfaces with an IFMS program. The IFMS program includes intervention subroutines that override the preprogrammed instructions that control the flight management computer. The intervention subroutines include a lateral (direction) control subroutine and several vertical subroutines. The vertical subroutines include altitude, speed and vertical path subroutines. The intervention subroutines can be engaged independently of one another. Control axes unrelated to an engaged intervention subroutine remain under the control of the preprogrammed flight management computer instructions.

Claims

1. In an airplane flight management system that includes a flight management computer that produces airplane speed and altitude control signals in accordacne with preprogrammed instructions, said speed and altitude control signals determining the route and profile of the airplane'"'"'s flight path, the improvement comprising an intervention flight management system (IFMS) integrated with said flight management computer for overriding said preprogrammed instructions, said IFMS comprising:

an IFMS control panel including manually position-adjustable knobs and switches, and related indicators, the position of said position-adjustable knobs and switches creating lateral and vertical flight path instructions; and

,

an IFMS control means coupled to said IFMS control panel for detecting the lateral and vertical flight path instructions created by the position of said position-adjustable knobs and switches and producing airplane speed and altitude control signals in accordance with said lateral and vertical flight path instructions that override contrary speed and altitude control signals produced by said flight management computer in response to said preprogrammed instructions.

2. The improvement claimed in claim 1 wherein said IFMS control means comprises an IFMS program.

3. The improvement claimed in claim 2 wherein said IFMS program is stored in said flight management computer.

4. The improvement claimed in claim 3 wherein:

said IFMS control panel includes a direction section, an altitude section, a speed section and a vertical path section; and

said IFMS program includes a direction subroutine, an altitude subroutine, a speed subroutine and a vertical path subroutine.

5. The improvement claimed in claim 4 wherein:

the direction section of said IFMS control panel includes a depressible and rotatable direction knob; and

,

said direction subroutine of said IFMS program monitors the depression status and rotatable position of said depressible and rotatable direction knob such that the depression status of said direction knob controls the engagement and disengagement status of said direction subroutine and the rotation position of said direction knob controls the direction of said airplane when said direction subroutines is engaged.

6. The improvement claimed in claim 5 wherein:

the direction section of said IFMS control panel also includes a heading/track select switch, said heading/track select switch being a toggle switch that alternates between heading and tract state each time said heading/track select switch is actuated; and

,

said direction subroutine of said IFMS program monitors the state of said heading/track select switch and includes alternate heading and track paths followed in accordance with the state of said heading/track select switch.

7. The improvement claimed in claim 5 wherein:

said altitude section of said IFMS control panel includes a depressible and rotatable altitude knob and an altitude display; and

,

said altitude subroutine of said IFMS program monitors the depression status and rotation position of said altitude knob such that the depression status of said altitude knob controls the altitude intervention input to said altitude subroutine and the rotational position of said altitude knob controls the altitude of said airplane.

8. The improvement claimed in claim 7 wherein:

said speed section of said IFMS control panel includes a depressible and rotatable speed knob; and

,

said speed subroutine of said IFMS program monitors the depression status and rotation position of said speed knob such that the depression status of said speed knob controls the engagement and disengagement status of said speed subroutine and the rotational position of said speed knob controls the speed of said airplane when said speed subroutine is engaged.

9. The improvement claimed in claim 8 wherein:

said speed section of said IFMS control panel also includes an IAS/MACH select switch, said IAS select switch being a toggle switch that alternates between IAS and MACH positions each time said IAS/MACH switch is actuated; and

,

said speed subroutine of said IFMS program monitors the state of said IAS/MACH select switch and includes alternate IAS and MACH paths followed in accordance with the state of said IAS/MACH select switch.

10. The improvement claimed in claim 8 wherein:

said vertical path section of said IFMS control panel includes a depressible and rotatable vertical path knob; and

,

said vertical path subroutine of said IFMS program monitors the depression status and rotatable position of said vertical path knob such that the depression status of said vertical path knob controls the engagement and disengagement status of said vertical path subroutine and the rotational position of said vertical path knob controls the direction and rate of climb or descent of said airplane when said vertical path subroutine is engaged.

11. The improvement claimed in claim 10 wherein:

said vertical path section of said IFMS control panel also includes a VS/FPA select switch, said VS/FPA select switch being a toggle switch that alternates between VS and FPA positions each time the VS/FPA select switch is actuated; and

,

said vertical path subroutine of said IFMS program monitors the state of said VS/FPA select switch and includes alternate VS and FPA paths followed in accordance with the state of said VS/FPA select switch.

12. The improvement claimed in claim 4 wherein:

said altitude section of said IFMS control panel includes a depressible and rotatable knob and an altitude display; and

,

said altitude subroutine of said IFMS program monitors the depression status and rotation position of said altitude knob such that the depression status of said altitude knob controls the altitude intervention input to said altitude subroutine and the rotational position of said altitude knob controls the altitude of said airplane when said altitude subroutine is engaged.

13. The improvement claimed in claim 12 wherein:

said speed section of said IFMS control panel includes a depressible and rotatable speed knob; and

,

said speed subroutine of said IFMS program monitors the depression status and rotation position of said speed knob such that the depression status of said speed knob controls the engagement and disengagement status of said speed subroutine and the rotational position of said speed knob controls the speed of said airplane when said speed subroutine is engaged.

14. The improvement claimed in claim 13 wherein:

said speed section of said IFMS control panel also includes an IAS/MACH select switch, said IAS select switch being a toggle switch that alternates between IAS and MACH positions each time said IAS/MACH switch is actuated; and

,

said speed subroutine of said IFMS program monitors the state of said IAS/MACH select switch and includes alternate IAS and MACH paths followed in accordance with the state of said IAS/MACH select switch.

15. The improvement claimed in claim 13 wherein:

said vertical path section of said IFMS control panel includes a depressible and rotatable vertical path knob; and

,

said vertical path subroutine of said IFMS program monitors the depression status and rotatable position of said vertical path knob such that the depression status of said vertical path knob controls the engagement and disengagement status of said vertical path subroutine and the rotational position of said vertical path knob controls the direction and rate of climb or descent of said airplane when said vertical path subroutine is engaged.

16. The improvement claimed in claim 15 wherein:

said vertical path section of IFMS control panel also includes a VS/FPA select switch, said VS/FPA select switch being a toggle switch that alternates between VS and FPA positions each time the VS/FPA select switch is actuated; and

,

said vertical path subroutine of said IFMS program monitors the state of said VS/FPA select switch and includes alternate VA and FPA paths followed in accordance with the state of said VS/FPA select switch.

17. The improvement claimed in claim 4 wherein:

said speed section of said IFMS control panel includes a depressible and rotatable speed knob; and

,

said speed subroutine of said IFMS program monitors the depression status and rotation position of said speed knob such that the depression status of said speed knob controls the engagement and disengagement status of said speed subroutine and the rotational position of said speed knob controls the speed of said airplane when said speed subroutine is engaged.

18. The improvement claimed in claim 17 wherein:

said speed section of said IFMS control panel also includes an IAS/MACH select switch, said IAS select switch being a toggle switch that alternates between IAS and MACH positions each time said IAS/MACH switch is actuated; and

,

said speed subroutine of said IFMS program monitors the state of said IAS/MACH select switch and includes alternate IAS and MACH paths followed in accordance with the state of said IAS/MACH select switch.

19. The improvement claimed in claim 17 wherein:

said vertical path section of said IFMS control panel includes a depressible and rotatable vertical path knob; and

,

said vertical path subroutine of said IFMS program monitors the depression status and rotatable position of said vertical path knob such that the depression status of said vertical path knob controls the engagement and disengagement status of said vertical path subroutine and the rotational position of said vertical path knob controls the direction and rate of climb or descent of said airplane when said vertical path subroutine is engaged.

20. The improvement claimed in claim 19 wherein:

said vertical path section of said IFMS control panel also includes a VS/FPA select switch, said VS/FPA select switch being a toggle switch that alternates between VA and FPA positions each time the VS/FPA select switch is actuated; and

,

said vertical path subroutine of said IFMS program monitors the state of said VS/FPA select switch and includes alternate VS and FPA paths followed in accordance with the state of said VS/FPA select switch.

21. The improvement claimed in claim 4 wherein:

said vertical path section of said IFMS control panel includes a depressible and rotatable vertical path knob; and

,

said vertical path subroutine of said IFMS program monitors the depression status and rotatable position of said vertical path knob such that the depression status of said vertical path knob controls the engagement and disengagement status of said vertical path subroutine and the rotational position of said vertical path knob controls the direction and rate of climb or descent of said airplane when said vertical path subroutine is engaged.

22. The improvement claimed in claim 21 wherein:

said vertical path section of said IFMS control panel also includes a VS/FPA select switch, said VS/FPA select switch being a toggle switch that alternates between VS and FPA positions each time the VS/FPA select switch is actuated; and

,

said vertical path subroutine of said IFMS program monitors the state of said VS/FPA select switch and includes alternate VS and FPA paths followed in accordance with the state of said VS/FPA select switch.