Projectile guidance with accelerometers and a GPS receiver
First Claim
1. A projectile guidance system with accelerometers and a GPS receiver comprising:
- a projectile having a triax of accelerometers mounted in the projectile and providing roll, pitch and azimuth axis acceleration data;
a GPS antenna and receiver means mounted in the projectile for providing and updating present position data;
a computer and memory mounted in the projectile and executing a guidance program; and
divert propulsion means;
wherein the guidance program is responsive to the roll, pitch and azimuth axis acceleration data and to the sampled present position data for calculating and outputting time indexed roll, pitch and azimuth angles, time indexed present position and velocity to a flight control system for guiding the projectile to a predetermined target location; and
wherein the divert propulsion means are responsive to the guidance program.
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Accused Products
Abstract
A projectile guidance system without gyros in which the projectile has an orthogonal body coordinate system. The projectile has a triax of accelerometers providing x, y and z acceleration data measured along the x, y and z axes respectively. A GPS antenna and receiver means provides onboard GPS position and velocity data in earth referenced navigational coordinates. A computer and program means stores and accesses time indexed GPS position and GPS velocity data and transforms x, y and z axis acceleration data from body to navigation coordinates. The program means is responsive to corresponding time indexed acceleration data and to GPS velocity and position data for calculating and outputting an estimated projectile roll, pitch and yaw angle via optimal smoothing techniques with respect to local level for each time index iteration of present position to a flight control system, which actuates a divert propulsion system for guiding the projectile to a predetermined location.
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Citations
20 Claims
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1. A projectile guidance system with accelerometers and a GPS receiver comprising:
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a projectile having a triax of accelerometers mounted in the projectile and providing roll, pitch and azimuth axis acceleration data;
a GPS antenna and receiver means mounted in the projectile for providing and updating present position data;
a computer and memory mounted in the projectile and executing a guidance program; and
divert propulsion means;
wherein the guidance program is responsive to the roll, pitch and azimuth axis acceleration data and to the sampled present position data for calculating and outputting time indexed roll, pitch and azimuth angles, time indexed present position and velocity to a flight control system for guiding the projectile to a predetermined target location; and
wherein the divert propulsion means are responsive to the guidance program. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18)
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19. A projectile guidance system without gyros comprising:
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the projectile having at least a triax of accelerometers comprising an x accelerometer for providing x-axis acceleration data measured along the x-axis, an accelerometer for providing y-axis acceleration data measured along the y-axis and a z-accelerometer for providing z-axis acceleration data measured along the z-axis, a GPS antenna and receiver means for providing onboard GPS position and GPS velocity data in earth referenced navigational coordinates, a computer and memory and program means for storing and accessing time indexed GPS position and GPS velocity data and for transforming the x, y and z axis acceleration data from body to navigation coordinates, the acceleration data being arrayed and having time indexes common with the GPS position and velocity data; and
divert propulsion responsive to the program means;
wherein the program means is responsive to correcting time indexed acceleration data and to GPS velosity and position data for calculating and outputting an estimated projectile roll, pitch and yaw angle with respect to local level for each time index iteration of present position, velocity and acceleration data to a flight control system for guiding the projectile to a predetermined target location.
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20. A projectile guidance system process for the guidance of a vehicle or projectile without gyros, the vehicle having been launched and having an orthogonal coordinate system with a longitudinal or x-axis for roll measurement, a y-axis for pitch measurement, and a z-axis for yaw measurement, a triax of accelerometers outputting x, y and z axis acceleration, and a GPS antenna and receiver means for providing GPS position and GPS velocity data in earth referenced navigational coordinates, the projectile guidance system process comprising the steps of:
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receiving, indexing and storing GPS position and velocity data with concurrent x, y and z axis acceleration data with a computer and memory means executing a program to calculate a trajectory for the vehicle as a function of a set of state equations, the program converting the x, y and z axis acceleration data to a local level navigational reference system, the program then solving a set of time indexed state equations to update the system'"'"'s estimated state, and then computing a time indexed pitch, roll and yaw angle in locally level coordinates, the program then outputting the time indexed pitch, roll yaw angle in locally level coordinates with a corresponding time indexed present position to a flight control system for guiding the projectile to a destination;
the flight control system controlling divert propulsion means to guide the vehicle or projectile.
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Specification