US4769759A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for developing air data for use in flight control systems
Assignee: Honeywell International Inc
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Filing: 1986-06-16
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Granted: 1988-09-06
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Expires: 2006-06-16
Abstract
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.
Inventors
- 👤 Mcgough John G.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 05:34
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/08; G05D1/0808; G05D1/0816; G05D1/0825
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
86 words
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.
Claim 2
Independent Claim
86 words
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.
Claim 3
Dependent Claim
101 words
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.
Claim 4
Dependent Claim
34 words
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.
Claim 5
Dependent Claim
49 words
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.
Claim 6
Independent Claim
107 words
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.
Claim 7
Independent Claim
107 words
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.
Claim 8
Dependent Claim
75 words
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.
Claim 9
Dependent Claim
34 words
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.
Claim 10
Dependent Claim
49 words
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.
Claim 11
Independent Claim
149 words
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.
Claim 12
Independent Claim
149 words
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.
References Cited (Backward Citations)
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1991-09-06 | 1992-03-07 | 1992-09-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-09-06 | 1996-03-07 | 1996-09-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-09-06 | 2000-03-07 | 2000-09-06 | $7700.00 | Window Closed / Lapsed |