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Class Information
Number: 244/191
Name: Aeronautics > Aircraft control > Automatic > Electric course control > Acceleration control
Description: System which governs the aircraft in response to a rate of change in speed thereof.
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 7146299 |
Adjustable simulation vehicle capabilities |
Dec. 5, 2006 |
| 6539290 |
Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation |
Mar. 25, 2003 |
| 6459228 |
Dual input servo coupled control sticks |
Oct. 1, 2002 |
| 6253481 |
Shotgun mountable shell holder |
Jul. 3, 2001 |
| 6189836 |
Model-following control system using acceleration feedback |
Feb. 20, 2001 |
| 6062513 |
Total energy based flight control system |
May. 16, 2000 |
| 6064923 |
Aircraft with reduced wing structure loading |
May. 16, 2000 |
| 5833173 |
Aircraft frequency adaptive modal suppression system |
Nov. 10, 1998 |
| 5815407 |
Method and device for inhibiting the operation of an electronic device during take-off and landing of an aircraft |
Sep. 29, 1998 |
| 5722620 |
Aircraft pitch-axis stability and command augmentation |
Mar. 3, 1998 |
| 5641136 |
Combat agility management system |
Jun. 24, 1997 |
| 5589749 |
Closed loop control system and method using back EMF estimator |
Dec. 31, 1996 |
| 5452865 |
Aircraft frequency adaptive modal suppression system |
Sep. 26, 1995 |
| 5248114 |
Adaptive autopilot |
Sep. 28, 1993 |
| 5224667 |
System enabling the flutter behavior of an aircraft to be improved |
Jul. 6, 1993 |
| 5186416 |
System for reducing the forces applied to the wings and particularly to the root of the wings of an aircraft in flight |
Feb. 16, 1993 |
| 5128671 |
Control device having multiple degrees of freedom |
Jul. 7, 1992 |
| 5058836 |
Adaptive autopilot |
Oct. 22, 1991 |
| 5053767 |
Aircraft windshear detection based on energy loss |
Oct. 1, 1991 |
| 4905934 |
Universal-type gust alleviation system for aircraft |
Mar. 6, 1990 |
| 4857922 |
Windshear detection and warning system with evasion command |
Aug. 15, 1989 |
| 4821981 |
Maneuver enchancement and gust alleviation system |
Apr. 18, 1989 |
| 4697768 |
Flight control system employing complementary filter |
Oct. 6, 1987 |
| 4651958 |
Method and apparatus for effecting fine control of aircraft velocity |
Mar. 24, 1987 |
| 4645144 |
Method and apparatus for effecting fine control of aircraft velocity |
Feb. 24, 1987 |
| 4593285 |
Windshear detection and warning system with evasion command |
Jun. 3, 1986 |
| 4562546 |
Stability augmentation system for a forward swept wing aircraft |
Dec. 31, 1985 |
| 4229725 |
Wind shear warning system for aircraft |
Oct. 21, 1980 |
| 4127249 |
Apparatus for computing the rate of change of energy of an aircraft |
Nov. 28, 1978 |
| 4095271 |
Aircraft pitch attitude signal generator |
Jun. 13, 1978 |
| 4079905 |
System for providing an indication of wind shear |
Mar. 21, 1978 |
| 4046341 |
Aircraft angle-of-attack and sideslip estimator |
Sep. 6, 1977 |
| 4012713 |
System for providing an indication of wind shear |
Mar. 15, 1977 |
| 3998411 |
Speed overshoot correction system |
Dec. 21, 1976 |
| 3979090 |
Velocity damped erection system for stable gyroscopic attitude and heading reference apparatus |
Sep. 7, 1976 |
| 3948096 |
Apparatus for computing the acceleration of an aircraft along its flight path |
Apr. 6, 1976 |
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