Method for developing air data for use in flight control systems

• US 4,769,759 A
• Filed: 06/16/1986
• Issued: 09/06/1988
• Est. Priority Date: 06/16/1986
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Alliedsignal Inc.
• Inventors: McGough John G.
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): Black Thomas G.
• Application Number:
  US06/874,761
• Time in Patent Office: 813 Days
• Field of Search: 364/434, 364/453, 364/435, 364/559, 364/565, 364/566, 244/178, 244/177, 244/181
• US Class Current: 701/6
• CPC Class Codes: G05D 1/0825 using mathematical models

Abstract

A method for developing desired air data for use in flight control systems is disclosed including determining angle of attack and sideslip angle relative to inertial space and also determining said angles by solving appropriate aerodynamic equations, whereby two independent estimates of the angles are provided. These estimates are combined for providing the desired data.

Claims

1. A method for developing desired estimates of angle of attack and sideslip angle for controlling the flight of an aircraft, comprising the steps of:

developing first estimates of angle of attack and sideslip angle relative to inertial space;

developing second estimates of angle of attack and sideslip angle based on aerodynamic force relationships; and

combining the first estimates and the second estimates for developing the desired estimates of angle of attack and sideslip angle and controlling the flight of the aircraft based on said desired estimates.

2. A method as described by claim 1, further comprising the steps of:

combining the desired estimates with the second estimates for providing first combined estimates;

applying a fixed gain to the first combined estimates;

filtering the first combined estimates having the fixed gain applied thereto;

combining the filtered, first combined estimates having the fixed gain applied thereto with the first estimates for providing second combined estimates, said second combined estimates being the desired estimates; and

said desired estimates corresponding to the first estimates at relatively high aircraft flight frequencies and corresponding to the second estimates at relatively low aircraft flight frequencies.

3. A method as described by claim 2, wherein combining the desired estimates with the second estimates for providing the first combined estimates is comprised of:

algebraically summing the desired estimates and the second estimates.

4. A method as described by claim 2, wherein combining the filtered, first combined estimates having the fixed gain applied thereto with the first estimates for providing the second combined estimates is comprised of:

adding the filtered, first combined estimate having the fixed gain applied thereto and the first estimates.

5. A method for developing desired estimates of angle of attack and sideslip angle for controlling the flight of an aircraft, comprising the steps of:

developing first estimates of angle of attack and sideslip angle relative to inertial space;

developing second estimates of angle of attack and sideslip angle based on aerodynamic force relationships; and

combining the first and second estimates for developing the desired estimates of angle of attack and sideslip angle and controlling the flight of the aircraft so that the desired estimates correspond to the first estimates at relatively high aircraft flight frequencies and correspond to the second estimates at relatively low aircraft flight frequencies.

6. A method as described by claim 5, further comprising the steps of:

combining the desired estimates with the second estimates for providing first combined estimates;

applying a fixed gain to the first combined estimates;

filtering the first combined estimates having the fixed gain applied thereto; and

combining the filtered, first combined estimates having the fixed gain applied thereto with the first estimates for providing second combined estimates, said second combined estimates being the desired estimate.

7. A method as described by claim 6, wherein combining the desired estimates with the second estimates for providing the first combined estimates is comprised of:

algebraically summing the desired estimates and the second estimates.

8. A method as described by claim 7, wherein combining the filtered, first combined estimates having the fixed gain applied thereto with the first estimates for providing the second combined estimates is comprised of:

adding the filtered, first combined estimates having the fixed gain applied thereto and the first estimates.

9. A method for developing desired estimates of angle of attack and sideslip angle for controlling the flight of an aircraft, comprising the steps of:

developing first estimates of angle of attack and sideslip angle relative to inertial space;

developing second estimates of angle of attack and sideslip angle based on aerodynamic force relationships;

algebraically summing the desired estimates and the second estimates for providing summed estimates;

applying a fixed gain to the summed estimates;

filtering the summed estimates having the fixed gain applied thereto;

adding the filtered, summed estimates having the fixed gain applied thereto to the first estimates for providing added estimates and controlling the flight of the aircraft based on said added estimates;

said added estimates being the desired estimates; and

said desired estimates corresponding to the first estimates at relatively high aircraft flight frequencies and corresponding to the second estimates at relatively low aircraft flight frequencies.