Optimization and Mechanization of Periodic Flight

• US 20090177339A1
• Filed: 01/16/2009
• Published: 07/09/2009
• Est. Priority Date: 03/03/2005
• Status: Abandoned Application

• Current Assignee: Jason L. Speyer, Robert H. Chen
• Original Assignee: Jason L. Speyer, Robert H. Chen
• Inventors: Speyer, Jason L., Chen, Robert H.
• Application Number:
  US12/355,473
• Publication Number:
  US 20090177339A1
• Time in Patent Office: Days
• US Class Current: 701/3
• CPC Class Codes: G05D 1/0005 with arrangements to save energy
• CPC Class Codes: G05D 1/101 specially adapted for aircraft
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0052 for cruising combined instruments indicating more than one navigational value G01C23/00

Abstract

The implementation of periodic flight for enhancing aircraft'"'"'s endurance or range is described having at least two components in the periodic flight embodiments. The first component is the trajectory optimization which determines the optimal periodic trajectory (such as altitude, velocity and flight path angle) that produces maximal endurance or range for a given fuel. The second component is the periodic guidance law which mechanizes the optimal periodic trajectory. For certain aircraft, periodic flight improves that aircraft'"'"'s endurance or range over steady state flight.

Claims

1. A machine-enabled method of periodic guidance for regulating an air vehicle about a periodic trajectory, the method comprising:

generating a plurality of trajectories comprising time-dependent values including;

a time history of one or more vehicle control command values, a plurality of vehicle state values comprising at least one vehicle velocity value, and at least one vehicle altitude value; and

wherein the generating of the plurality of trajectories is based on minimizing a predicted fuel consumption per time value using a machine-executable vehicle model, wherein the machine-executable vehicle model includes a lift coefficient and a drag coefficient, and wherein the lift coefficient value and the drag coefficient value are based on a vehicle state value and a vehicle control command value;

generating the periodic trajectory from a portion of at least one of the plurality of generated trajectories comprising the time-dependent values, the periodic trajectory derivation based on a current vehicle state and a current vehicle mass; and

generating one or more air vehicle control system commands based on the output generated periodic trajectory comprising time-dependent values including at least the time history of one or more vehicle control command values.

2. The machine-enabled method of periodic guidance of claim 1 wherein the step of generating a plurality of trajectories is based on a predicted straight line horizontal vehicle flight path.

3. The machine-enabled method of periodic guidance of claim 1 wherein the step of generating a plurality of trajectories is based on a predicted circular horizontal flight path.

4. The machine-enabled method of periodic guidance of claim 1 further comprising, following the step of generating a plurality of trajectories, storing one or more of the plurality of trajectories via a recordable medium configured for stored trajectory retrieval.

5. The machine-enabled method of periodic guidance of claim 1 wherein the step of generating the periodic trajectory from the portion of at least one of the plurality of generated trajectories further comprises interpolating across portions of two or more of the plurality of generated trajectories, and generating the periodic trajectory based on the interpolated portions of the plurality of generated trajectories.

6. The machine-enabled method of periodic guidance of claim 1 wherein the step of generating the periodic trajectory from the portion of at least one of the plurality of generated trajectories further comprises interpolating across portions of two or more of the plurality of generated trajectories using a learning architecture, and generating the periodic trajectory based on the interpolated portions of the plurality of generated trajectories.

7. The machine-enabled method of periodic guidance of claim 1 wherein the step of generating the periodic trajectory from at least one of the plurality of generated trajectories further comprises the periodic trajectory generation based on the current vehicle state, the current vehicle mass, and at least one way point command comprising at least one of latitude, longitude, or altitude.

8. The machine-enabled method of periodic guidance of claim 1 wherein the step of generating a plurality of trajectories using a finite number of control variables is based on at least two values for each control variable.

9. A system for operating an air vehicle along a periodic trajectory comprising:

a navigation computing subsystem configured to estimate the plurality of vehicle states;

a guidance computing subsystem having a computer processor and addressable member, the guidance computing subsystem configured to execute machine-readable instructions to;

generate a plurality of trajectories comprising time-dependent values including at least;

a time history of one or more vehicle control command values, a plurality of vehicle state values comprising at least one vehicle velocity value, and at least one vehicle altitude value; and

wherein the generation of the plurality of trajectories is based on minimizing a predicted fuel consumption per time value using a machine-executable vehicle model, wherein the machine-executable vehicle model includes at least a lift coefficient and a drag coefficient, and wherein the lift coefficient value and the drag coefficient value are based on a vehicle state value and a vehicle control command value;

generate the periodic trajectory from a portion of at least one of the plurality of generated trajectories comprising the time-dependent values, wherein the periodic trajectory generation is based on a current vehicle state and a current vehicle mass; and

generate one or more air vehicle control system commands based on the output generated periodic trajectory comprising time-dependent values including the time history of one or more vehicle control command values.

10. The system of claim 9 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate a plurality of trajectories based on a predicted straight line horizontal vehicle flight path.

11. The system of claim 9 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate a plurality of trajectories based on a predicted circular horizontal flight path.

12. The system of claim 9 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate the periodic trajectory from portions of two or more of the plurality of generated trajectories by interpolating across the portions of two or more of the plurality of generated trajectories.

13. The system of claim 9 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate the periodic trajectory from portions of two or more of the plurality of generated trajectories by interpolating across the portions of two or more of the plurality of generated trajectories using a learning architecture.

14. The system of claim 9 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to store one or more of the plurality of generated trajectories via a recordable medium configured for trajectory selection.

15. The system of claim 9 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate the periodic trajectory from portions of two or more of the plurality of generated trajectories by interpolating across two or more of the plurality of generated trajectories using an averaging scheme.

16. The system of claim 9 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate the periodic trajectory, the periodic trajectory generation instructions based on the current vehicle state, the current vehicle mass, and at least one way point command comprising at least one of latitude, longitude, or altitude.

17. The system of claim 9 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate a plurality of trajectories based upon the finite number of control variables limited to at least two values for each control variable.

18. A machine-enabled method of periodic guidance for regulating an air vehicle about a periodic trajectory, the method comprising:

generating a plurality of trajectories comprising time-dependent values including;

a time history of one or more vehicle control command values, a plurality of vehicle state values comprising at least one vehicle velocity value, and at least one vehicle altitude value; and

wherein the generating of the plurality of trajectories is based on maximizing a predicted down range value using a machine-executable vehicle model, wherein the machine-executable vehicle model includes a lift coefficient and a drag coefficient, and wherein the lift coefficient value and the drag coefficient value are based on a vehicle state value and a vehicle control command value;

generating the periodic trajectory from a portion of at least one of the plurality of generated trajectories comprising the time-dependent values, the periodic trajectory derivation based on a current vehicle state and a current vehicle mass; and

generating one or more air vehicle control system commands based on the output generated periodic trajectory comprising time-dependent values including at least the time history of one or more vehicle control command values.

19. The machine-enabled method of periodic guidance of claim 18 wherein the generating of the plurality of trajectories is based on maximizing a predicted down range per unit fuel consumed value.

20. The machine-enabled method of periodic guidance of claim 18 wherein the step of generating a plurality of trajectories is based on a predicted straight line horizontal vehicle flight path.

21. The machine-enabled method of periodic guidance of claim 18 wherein the step of generating a plurality of trajectories is based on a predicted circular horizontal flight path.

22. The machine-enabled method of periodic guidance of claim 18 further comprising, following the step of generating a plurality of trajectories, storing one or more of the plurality of trajectories via a recordable medium configured for stored trajectory retrieval.

23. The machine-enabled method of periodic guidance of claim 18 wherein the step of generating the periodic trajectory from the portion of at least one of the plurality of generated trajectories further comprises interpolating across portions of two or more of the plurality of generated trajectories, and generating the periodic trajectory based on the interpolated portions of the plurality of generated trajectories.

24. The machine-enabled method of periodic guidance of claim 18 wherein the step of generating the periodic trajectory from the portion of at least one of the plurality of generated trajectories further comprises interpolating across portions of two or more of the plurality of generated trajectories using a learning architecture, and generating the periodic trajectory based on the interpolated portions of the plurality of generated trajectories.

25. The machine-enabled method of periodic guidance of claim 18 wherein the step of generating the periodic trajectory from at least one of the plurality of generated trajectories further comprises the periodic trajectory generation based on the current vehicle state, the current vehicle mass, and at least one way point command comprising at least one of latitude, longitude, or altitude.

26. The machine-enabled method of periodic guidance of claim 18 wherein the step of generating a plurality of trajectories using a finite number of control variables is based on at least two values for each control variable.

27. A system for operating an air vehicle along a periodic trajectory comprising:

a navigation computing subsystem configured to estimate the plurality of vehicle states;

a guidance computing subsystem having a computer processor and addressable member, the guidance computing subsystem configured to execute machine-readable instructions to;

generate a plurality of trajectories comprising time-dependent values including at least;

a time history of one or more vehicle control command values, a plurality of vehicle state values comprising at least one vehicle velocity value, and at least one vehicle altitude value; and

wherein the generation of the plurality of trajectories is based on maximizing a predicted down range value using a machine-executable vehicle model, wherein the machine-executable vehicle model includes at least a lift coefficient and a drag coefficient, and wherein the lift coefficient value and the drag coefficient value are based on a vehicle state value and a vehicle control command value;

generate the periodic trajectory from a portion of at least one of the plurality of generated trajectories comprising the time-dependent values, wherein the periodic trajectory generation is based on a current vehicle state and a current vehicle mass; and

generate one or more air vehicle control system commands based on the output generated periodic trajectory comprising time-dependent values including the time history of one or more vehicle control command values.

28. The system of claim 27 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate a plurality of trajectories based on maximizing a predicted down range per unit fuel consumed value.

29. The system of claim 27 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate a plurality of trajectories based on a predicted straight line horizontal vehicle flight path.

30. The system of claim 27 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate a plurality of trajectories based on a predicted circular horizontal flight path.

31. The system of claim 27 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate the periodic trajectory from portions of two or more of the plurality of generated trajectories by interpolating across the portions of two or more of the plurality of generated trajectories.

32. The system of claim 27 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate the periodic trajectory from portions of two or more of the plurality of generated trajectories by interpolating across the portions of two or more of the plurality of generated trajectories using a learning architecture.

33. The system of claim 27 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to store one or more of the plurality of generated trajectories via a recordable medium configured for trajectory selection.

34. The system of claim 27 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate the periodic trajectory from portions of two or more of the plurality of generated trajectories by interpolating across two or more of the plurality of generated trajectories using an averaging scheme.

35. The system of claim 27 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate the periodic trajectory, the periodic trajectory generation instructions based on the current vehicle state, the current vehicle mass, and at least one way point command comprising at least one of latitude, longitude, or altitude.

36. The system of claim 27 wherein the guidance computing subsystem is further configured to execute machine-readable instructions to generate a plurality of trajectories based upon the finite number of control variables limited to at least two values for each control variable.