Projectile steering apparatus and method

• US 4,966,078 A
• Filed: 12/27/1989
• Issued: 10/30/1990
• Est. Priority Date: 03/20/1987
• Status: Expired due to Fees

• Current Assignee: Lars J. Schleimann-Jensen
• Original Assignee: Lars J. Schleimann-Jensen
• Inventors: Schleimann-Jensen, Lars J.
• Primary Examiner(s): BROWN, DAVID
• Application Number:
  US07/456,145
• Time in Patent Office: 307 Days
• Field of Search: 102/384, 102/388, 244/3.21, 244/3.24, 244/3.27, 244/3.28
• US Class Current: 102/384
• CPC Class Codes: F42B 10/58 of rotochute type
• CPC Class Codes: F42B 10/62 Steering by movement of flight surfaces

Abstract

Projectile steering apparatus and method employing the autogiro principle. Two rotatable blades are swung out from a longitudinal slot in a flying projectile. The blades are shaped to rotate as a result of the air stream rushing past the projectile. Steering is effected by altering the orientation of the blades with respect to the projectile in synchronism with rotation of the projectile. By varying the autogiro pattern produced by the pair of blades, it is possible to impart a force for correcting the projectile trajectory.

Claims

1. An apparatus for steering a projectile comprising:

a seeker for deriving an error signal identifying an error between a trajectory of said projectile and a desired trajectory;

a pair of rotor blades supported on a rear section of said projectile, said rotor blades rotating with said rear section;

means connected to said rotor blades for varying the angular position of said blades with respect to said projectile longitudinal axis in synchronism with rotation of said rear section, whereby a non-symmetrical power pattern is produced by said rotor blades, imparting a steering force to said projectile; and

control system means connected to said seeker for receiving said error signal, and for providing a control signal to said means for varying the angular position of said blades for producing a period variation of said blade position, whereby a force is applied to said projectile in a direction for reducing said error.

2. The apparatus of claim 1 wherein said means for varying the angular position of said blades comprises:

a linear actuator connected to said rear section, having an actuating arm connected to one end of one of said rotor blades; and

,

a pivot means located between said one end of said one rotor blade and a remaining end, permitting said one rotor blade to be angularly positioned with respect to said projectile axis.

3. An apparatus for steering a projectile comprising:

a seeker for deriving an error signal identifying an error between a trajectory of said projectile and a desired trajectory;

a pair of rotor blades supported on a rear section of said projectile, said rotor blades rotating with said rear section;

means connected to said rotor blades for rotating said rotor blades about their longitudinal axes while maintaining said longitudinal axis fixed with respect to said projectile longitudinal axis, whereby a lateral force may be imparted to said projectile for reducing said error; and

,

a control system connected to said seeker and to said means for rotating said rotor blades for providing a signal for rotating said rotor blades in synchronism with rotation of said axis, to create a power pattern from said rotor blades which applies a lateral force to said projectile in a direction which reduces said error.

4. The apparatus of claim 3 wherein said means for rotating said rotor blades comprises:

an axle connected to one of said rotor blades supporting said rotor blade for rotation along a longitudinal axis;

a linkage arm having one end connected to said blade, and a second end for receiving a force for rotating said axle and connected blade; and

,

a linear actuator having an actuating arm connected to said linkage arm second end, receiving a signal from said control system which rotates said blades in synchronism with said projectile rotation.

5. A method for steering a projectile comprising:

providing at a rear of said projectile a pair of rotor blades which rotate with said projectile, and which are angularly displaceable from the longitudinal axis of said projectile;

determining a trajectory error for said projectile; and

,

varying the angular position of said blades with respect to the longitudinal axis of said projectile in synchronism with rotation of said projectile, whereby said rotor blades generate a power pattern which produces a lateral force on said projectile in a direction to reduce said trajectory error.