System for facilitating control of an aircraft

• US 20110184593A1
• Filed: 04/19/2007
• Published: 07/28/2011
• Est. Priority Date: 04/19/2006
• Status: Abandoned Application

• Current Assignee: John M. Swope
• Original Assignee: John M. Swope
• Inventors: Swope, John M.
• Application Number:
  US11/788,715
• Publication Number:
  US 20110184593A1
• Time in Patent Office: Days
• US Class Current: 701/12
• CPC Class Codes: G05D 1/106 Change initiated in response to external conditions, e.g. avoidance of elevated terrain or of no-fly zones

Abstract

A system for providing flight control instructions to an aircraft is claimed, wherein using aircraft position or velocity data, an outer control loop algorithm determines an aircraft target angle and an inner control loop algorithm outputs commands to cause the aircraft to achieve the target angle. Utilizing the commands outputted from the control loops, aircraft are able to autonomously take-off and land, station hold in a very precise manner, and fly in very close proximity to other objects with little chance of collision.

Claims

1. A method of providing flight control instructions to an aircraft, the method comprising the steps of:

a.

b. receiving a command to maintain a position and/or velocity relationship to at least one object wherein a distance between said at least one object and said aircraft is less than 2000 feet;

c. utilizing at least two control loop algorithms, in which an outer control loop algorithm determines an aircraft target angle and an inner control loop algorithm outputs commands, to cause said aircraft to achieve said aircraft target angle;

d. utilizing optic flow data from a sensor system capable of detecting optic flow;

e. utilizing vertical reference data derived from the combination of data from at least accelerometers and angular rate gyros; and

f. combining data from said optic flow data and said vertical reference data, and utilizing said control algorithms to obtain said position and/or velocity relationship between aircraft and said at least one object.

2. The method of providing flight control instructions to an aircraft according to claim 1 wherein said relationship is defined as substantially zero translational drift relative to said at least one object, the method further comprising the step of:

a. determining the position of said aircraft corresponding to the aircraft'"'"'s current coordinates in at least two dimensions relative to said at least one object; and

b. wherein said position influences said aircraft target angle.

3. The method of providing flight control instructions to an aircraft according to claim 2, the method further comprising the step of:

b. modifying said aircraft target angle such that said aircraft resists external wind forces.

4. The method of providing flight control instructions to an aircraft according to claim 2, wherein said position is a first position, the method further comprising the steps of:

a. encountering a force external to said aircraft which moves said aircraft from said first position to a second position in said at least two dimensions; and

b. autonomously returning said aircraft to said first position from said second position, wherein said autonomously returning step occurs after said moving step.

5. The method of providing flight control instructions to an aircraft according to claim 2, the method further comprising the step of substantially maintaining said position while the altitude of said aircraft is modified.

6. The method of providing flight control instructions to an aircraft according to claim 1 wherein:

a. said at least one object has a relative velocity to said aircraft;

b. said relationship is defined as said relative velocity;

c. and said relative velocity influences said aircraft target angle.

7. The method of providing flight control instructions to an aircraft according to claim 6, the method further comprising the step of substantially maintaining said relative velocity while the altitude of said aircraft is modified.

8. The method of providing flight control instructions to an aircraft according to claim 6, the method further comprising the steps of:

a. receiving a user velocity command that commands said aircraft to maintain a substantially constant velocity relative to said at least one object;

b. calculating a scaled velocity command from said user velocity command;

c. calculating a target attitude angle for said aircraft wherein said calculations are influenced from at least one of either of said optic flow derived data set and a GPS derived data set; and

d. wherein as said distance increases, the amount of influence of said GPS derived data increases and the amount of influence of said optic flow derived data set decreases.

9. The method of providing flight control instructions to an aircraft according to claim 8, the method further comprising the step of substantially maintaining said relative velocity while the altitude of said aircraft is modified.

10. The method of providing flight control instructions to an aircraft according to claim 6, the method further comprising the steps of:

a. obtaining GPS movement data from a GPS system;

b. calculating a target attitude angle for said aircraft wherein said calculations are influenced from at least one of either of said GPS movement data and said optic flow derived data set; and

c. wherein as said distance increases, the amount of influence of said GPS movement data increases and the amount of influence of said optic flow derived data set decreases.

11. A method of controlling an aircraft, the method comprising the steps of:

a. calculating instantaneous aircraft movement data using a computer onboard the aircraft; and

b. continually calculating flight control data using at least two flight control loop algorithms in which an outer flight control loop algorithm determines an aircraft target angle and an inner flight control loop algorithm outputs commands to cause said aircraft to achieve said aircraft target angle.

c. Utilizing optic flow data from a sensor system capable of detecting optic flow.

d. Utilizing vertical reference data derived from the combination of data from at least accelerometers and angular rate gyros.

12. The method of controlling an aircraft according to claim 11 wherein said aircraft movement data comprises aircraft position data.

13. The method of controlling an aircraft according to claim 11 wherein said aircraft movement data comprises aircraft velocity data.

14. The method of controlling an aircraft according to claim 13, wherein said instantaneous aircraft movement data is derived from multiple sources, one of which is a GPS system and another which is said optic flow, the method further comprising the steps of:

a. providing an aircraft with said sensor oriented such that the principal object(s) in the field of view is the round underneath the aircraft;

b. obtaining GPS movement data from a GPS system wherein in-the calculations of said outer flight control loop algorithm is influenced from at least one of either of said GPS movement data and said optic flow data; and

c. wherein as the altitude of said aircraft increases, the amount of influence of said GPS movement data increases and the amount of influence of said optic flow data decreases.

15. The method of providing flight control instructions to an aircraft according to claim 13 further comprising the steps of:

a. receiving a user velocity command that commands said aircraft to maintain a substantially constant velocity relative to at least one object;

b. calculating a scaled velocity command from said user velocity command;

c. calculating a target attitude angle for said aircraft wherein said calculations are influenced from at least one of either of said scaled velocity command and said optic flow derived data set; and

d. wherein as the altitude of said aircraft increases, the amount of influence of said scaled velocity command increases and the amount of influence of said aircraft velocity data decreases.

16. A method for determining flight control data for an aircraft as a function of altitude to achieve smooth flight for the aircraft, the method comprising the steps of:

a. providing an aircraft flying at a distance from an object;

b. calculating the trajectory of said aircraft from at least one of either a translation-sensor derived data set and a GPS derived data set, wherein said calculating is influenced by at least one of said two data sets;

c. wherein each of said two data sets provides an amount of influence on said trajectory calculation; and

d. whereinas said distance increases, the amount of influence of said GPS derived data increases and the amount of influence of said optic flow derived data decreases;

e. utilizing optic flow data from a sensor system capable of detecting optic flow;

f. utilizing vertical reference data derived from the combination of data from at least accelerometers and angular rate gyros.

17. The method for determining flight control data for an aircraft as a function of altitude to achieve smooth flight for the aircraft according to claim 16, the method comprising the steps of:

a. utilizing at least two control loop algorithms in which an outer control loop algorithm determines an aircraft target angle and an inner control loop algorithm outputs commands to cause said aircraft to achieve said aircraft target angle.