Aeronautics and astronautics – Missile stabilization or trajectory control – Stabilized by rotation
Reexamination Certificate
2002-04-17
2003-07-15
Gregory, Bernarr E. (Department: 3662)
Aeronautics and astronautics
Missile stabilization or trajectory control
Stabilized by rotation
C244S003100, C244S003150, C244S003190, C701S207000, C701S213000, C342S357490, C342S357490
Reexamination Certificate
active
06592070
ABSTRACT:
BACKGROUND OF THE INVENTION
This invention relates to guidance of rotating vehicles, GPS guidance of artillery shells, and more specifically interference-aided navigation using interference signals.
Spinning vehicles such as artillery shells, missiles, bombs, and uninhabited aerial vehicles (UAV) are using navigation and guidance techniques to accurately reach their designated targets. Techniques in use include inertial navigation, global positioning system (GPS) guidance, and magnetic field sensing.
In many applications, such as artillery shell or missile guidance, the vehicle to be guided is spinning rapidly. The small size and high rotation rate of the vehicle greatly complicate traditional navigation enhancement techniques such as inertial aiding and multi-antenna beam forming as described in co-pending application 01CR040/KE, Ser. No. 10/005,237, filed Dec. 5, 2001. The small size of an artillery shell or fuse does not permit the use of large antenna arrays or complex RF electronics. Inertial navigation is very difficult to implement because even very small scale factor errors and instabilities lead to large and rapidly Increasing attitude errors. For example, a shell spinning at 250 Hz is turning at 90,000°/s. A scale factor error of only 11 ppm will cause an attitude error rate of 1°/s. The small gyros that could be packaged into an artillery round or fuse do not have the precision to maintain an accurate attitude estimate at these rotation rates. Traditionally, guided shell designers have been forced to resort to mechanical de-spinning systems that add cost, size, and complexity. Shells that are not de-spun have utilized omnidirectional antennas with limited jamming immunity for GPS signal reception, and no inertial aiding.
U.S. Pat. No. 6,208,936 describes some of the difficulties encountered in creating an effective navigation system for a rapidly spinning vehicle such as an artillery shell. A system is disclosed that utilizes a magnetic field sensor for tracking the rotation angle of the vehicle and a system for computationally de-spinning the vehicle to greatly simplify calculation and improve accuracy of the navigation solution. U.S. Pat. No. 6,163,021 also discloses utilizing a magnetic field sensor to de-spin the body-axis frame measurements and, in addition, using accelerometers to measure the Coriolis accelerations due to rotation. The need for gyros and their associated rate range and scale factor limitations is eliminated. The technique of utilizing accelerometers to measure rotation rate, in a spinning frame, is well known and disclosed in U.S. Pat. No. 4,520,669.
Use of a magnetic sensor for roll determination in a spinning vehicle can be effective under the correct circumstances. However, this approach requires the addition of a magnetic sensor and performance can be dependent on the magnetic properties of the vehicle and its electrical systems as well as its position on the earth and the magnetic environment. For example, near the equator a vehicle traveling approximately due north or south will have difficulty in determining its rotation angle.
Cited co-pending application Ser. No. 09/1879,392, filed Jun. 12, 2001, now U.S. Pat. No. 6,520,448, describes an advanced spinning-vehicle navigation (AVSN) system utilizing GPS or similar navigation signals to determine the rotation angle of the vehicle. This approach offers significant improvement in performance and robustness under interference once the navigation signals are acquired. However, the application does not describe any technique to enhance initial acquisition under high levels of jamming or interference.
Artillery navigation systems have utilized omnidirectional antennas to reduce the phase and amplitude modulation as a function of projectile roll angle. This approach has poor performance under conditions of interference and jamming because the GPS signal and interference source are continuously received at the same relative gain. The use of a directional antenna will tend to improve interference immunity because the GPS receiver's AGC control will tend to reduce gain when the antenna is pointed toward the jamming source, and tend to increase the gain when the antenna is pointed away from the interference. Unfortunately the directional antennas tend to produce large phase modulations with rotation, and performance is not fully optimized because the received signal is still being processed during the times when the antenna is pointed toward the jammer and signal to noise ratios may be close to zero.
The phase and amplitude modulation, combined with any external interference and jamming signal sources can make it difficult to acquire and track low-level navigation signals such as GPS. A practical, cost-effective, technique is needed for spinning vehicles to acquire and track low-level signals in the presence of large interference or jamming signals.
SUMMARY OF THE INVENTION
An interference-aided signal navigation system for a rotating vehicle to provide a rotation angle estimate is disclosed. The system includes an antenna that receives interference signals and desired navigation signals. A RF processing function connected to the antenna processes the received interference signals and the desired navigation signals into IF signals. An A/D converter connected to the RF processing function digitizes the interference signals and desired navigation signals to provide a digitized IF signal. A tracking filter tracks amplitude variations of the interference signals and provides a rotation angle estimate signal of the rotating vehicle.
An intensity detector connected to the RF processing function and the tracking filter may be used for determining the level of the interfering signal and for providing an input modulation signal to the tracking filter. An AGC loop connected to the A/D converter and to the tracking filter may provide an input modulation signal to the tracking filter.
The tracking filter may further comprise a first mixer for receiving the input modulation signal from the AGC loop and mixing the input modulation signal with a first demodulation signal. A first filter in the tracking filter filters the first mixer output signal to provide a phase error feedback signal. A tracking servo receives the phase error feedback signal, provides the first demodulation signal and provides the rotation angle estimate signal.
It is an object of the present invention to provide acquisition of navigation and other signals in spinning vehicles.
It is an object of the present invention to provide a system that acquires and tracks low-level signals in the presence of large interference and jamming signals.
It is a feature of the present inventions to utilize the amplitude modulation of any present interference signal to aid in the determination of vehicle rotation rate to aid in the acquisition of navigation and other signals.
It is a advantage of the present invention obtain roll angle estimates using interference or jamming signals from an interference tracking loop.
REFERENCES:
patent: 3765621 (1973-10-01), Shigehara
patent: 3834653 (1974-09-01), Perkel
patent: 4062509 (1977-12-01), Muhlfelder et al.
patent: 4347996 (1982-09-01), Grosso
patent: 4520669 (1985-06-01), Rider
patent: 4831544 (1989-05-01), Hojo et al.
patent: 5114094 (1992-05-01), Harris
patent: 5442560 (1995-08-01), Kau
patent: 5497704 (1996-03-01), Kurschner et al.
patent: 5740986 (1998-04-01), Seidensticker et al.
patent: 5809457 (1998-09-01), Yee et al.
patent: 6163021 (2000-12-01), Mickelson
patent: 6208936 (2001-03-01), Minor et al.
patent: 6398155 (2002-06-01), Hepner et al.
Co-filed patent application entitled “Interference-Aided Navigation With Temporal Beam Forming In Rotating Vehicles” filed on an even date, inventor J. Doty.
Co-pending patent application entitled “Spinning—Vehicle Navigation Using Apparent Modulation Of Navigational Signals” filed on Jun. 12, 2001, Application No. 09/879,392, inventors J. Doty and G. McGraw.
Co-pending patent application entitled “Low Cost Interference Reduction System For GPS Receivers” filed
Eppele Kyle
Gregory Bernarr E.
Jensen Nathan O.
Rockwell Collins, Inc.
LandOfFree
Interference-aided navigation system for rotating vehicles does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Interference-aided navigation system for rotating vehicles, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Interference-aided navigation system for rotating vehicles will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-3073195