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Class Information
Number: 244/3.2
Name: Aeronautics > Missile stabilization or trajectory control > Automatic guidance > Inertial
Description: Subject matter in which automatic guidance is achieved by means of self-contained automatic controlling devices that respond to acceleration producing forces.
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 7409292 |
Method and system for degimbalization of vehicle navigation data |
Aug. 5, 2008 |
| 7328104 |
Systems and methods for improved inertial navigation |
Feb. 5, 2008 |
| 7305286 |
System and method for gyro enhanced vertical flight information |
Dec. 4, 2007 |
| 7248967 |
Autonomous velocity estimation and navigation |
Jul. 24, 2007 |
| 7105790 |
Process to control the trajectory of a spinning projectile |
Sep. 12, 2006 |
| 7076342 |
Attitude sensing apparatus for determining the attitude of a mobile unit |
Jul. 11, 2006 |
| 7043343 |
Method for testing a missile time-space-position unit for missile |
May. 9, 2006 |
| 6948367 |
Dual bridge angular and linear accelerometer |
Sep. 27, 2005 |
| 6928876 |
Dual flexure plate angular accelerometer |
Aug. 16, 2005 |
| 6895817 |
Dual bridge angular accelerometer |
May. 24, 2005 |
| 6725173 |
Digital signal processing method and system thereof for precision orientation measurements |
Apr. 20, 2004 |
| 6714866 |
Methods and apparatus for installation alignment of equipment |
Mar. 30, 2004 |
| 6679457 |
Reaction wheel system with vernier control rotor |
Jan. 20, 2004 |
| 6666410 |
Load relief system for a launch vehicle |
Dec. 23, 2003 |
| 6654685 |
Apparatus and method for navigation of an aircraft |
Nov. 25, 2003 |
| 6621059 |
Weapon systems |
Sep. 16, 2003 |
| 6596976 |
Method and system for pointing and stabilizing a device |
Jul. 22, 2003 |
| 6573486 |
Projectile guidance with accelerometers and a GPS receiver |
Jun. 3, 2003 |
| 6496779 |
Inertial measurement unit with magnetometer for detecting stationarity |
Dec. 17, 2002 |
| 6380526 |
Employing booster trajectory in a payload inertial measurement unit |
Apr. 30, 2002 |
| 6349652 |
Aeroballistic diagnostic system |
Feb. 26, 2002 |
| 6314886 |
Projectile to be fired from a weapon barrel and stabilized by a guide assembly |
Nov. 13, 2001 |
| 6317688 |
Method and apparatus for achieving sole means navigation from global navigation satelite systems |
Nov. 13, 2001 |
| 6163021 |
Navigation system for spinning projectiles |
Dec. 19, 2000 |
| 6131068 |
Accuracy of an inertial measurement unit |
Oct. 10, 2000 |
| 6107616 |
Power failure interrupt recovery for the pendulous oscillating gyroscopic accelerometer (POGA) |
Aug. 22, 2000 |
| 6037899 |
Method for vectoring active or combat projectiles over a defined operative range using a GPS-supported pilot projectile |
Mar. 14, 2000 |
| 5948045 |
Method for airbourne transfer alignment of an inertial measurement unit |
Sep. 7, 1999 |
| 5886286 |
Monitoring safety system |
Mar. 23, 1999 |
| 5886339 |
Missile attitude safing system |
Mar. 23, 1999 |
| 5804812 |
Multiple node lambert guidance system |
Sep. 8, 1998 |
| 5739787 |
Vehicle based independent tracking system |
Apr. 14, 1998 |
| 5721680 |
Missile test method for testing the operability of a missile from a launch site |
Feb. 24, 1998 |
| 5660356 |
System for providing power and roll motion stability in a vehicle |
Aug. 26, 1997 |
| 5660355 |
Angle only range estimator for homing missile |
Aug. 26, 1997 |
| 5647558 |
Method and apparatus for radial thrust trajectory correction of a ballistic projectile |
Jul. 15, 1997 |
| 5451014 |
Self-initializing internal guidance system and method for a missile |
Sep. 19, 1995 |
| 5397079 |
Process for the autonomous positional control of guided missiles |
Mar. 14, 1995 |
| 5360184 |
High-performance, low-cost inertial guidance system |
Nov. 1, 1994 |
| 5274314 |
Adaptive friction compensator |
Dec. 28, 1993 |
| 5260709 |
Autonomous precision weapon delivery using synthetic array radar |
Nov. 9, 1993 |
| 5150856 |
System for aligning the inertial unit of a carried vehicle on that of a carrier vehicle |
Sep. 29, 1992 |
| 5065956 |
Method for detecting changes in spin rate of a missile in flight |
Nov. 19, 1991 |
| 5020745 |
Reaction wheel fricton compensation using dither |
Jun. 4, 1991 |
| 5001647 |
Inertial transformation matrix generator |
Mar. 19, 1991 |
| H710 |
Horizon reference system for a rotating body |
Nov. 7, 1989 |
| 4831544 |
Attitude and heading reference detecting apparatus |
May. 16, 1989 |
| 4791850 |
Electromagnetic launching system for long-range guided munitions |
Dec. 20, 1988 |
| 4791573 |
State-deviation-estimation circuit employing a phase-locked-loop phase reference |
Dec. 13, 1988 |
| 4783744 |
Self-adaptive IRU correction loop design interfacing with the target state estimator for multi-mode terminal handoff |
Nov. 8, 1988 |
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