Attitude-controlling system and a missile equipped with such a system

Claim 3

A system according to claim 1, in which the fins of the empennage are set in position on the cylindrical part of the empennage so as to form a substantially zero angle with the longitudinal axis of the body.

Claim 4

A system according to claim 1, in which the fins of the empennage are set in position on the cylindrical part of the body, at an angle to the longitudinal axis of the body which is other than zero and is between zero and five degrees.

Claim 5

A system according to claim 1, wherein said torque transmitter is an electrical torque motor.

Claim 6

A system according to claim 1, wherein the fins of the empennage are foldable fins which can be folded into the cylindrical part of the empennage prior to firing, that is, setting the body in motion, and unfolded upon firing.

Claim 7

A missile which includes a system for controlling the attitude of the missile when the missile is moving in a fluid, said system being capable of controlling the attitude of the missile in roll and comprising: a finned rotary empennage concentric with the missile; a bi-directional torque transmitter providing a connection between the missile and the empennage and acting on the empennage relative to the missile; an attitude detector means for producing a signal proportional to the divergence between the detected and desired attitudes of the missile; an amplifier means for amplifying said signal, said torque transmitter being connected to be driven by the amplified signal produced by said amplifier means; and a source of electrical energy for powering said amplifier and said bi-directional torque transmitter.

Claim 8

A missile which includes a system for controlling the attitude of the missile when the missile is moving in a fluid, said system being capable of controlling the attitude of the missile in roll and comprising: a finned rotary empennage concentric with the missile; a bi-directional torque transmitter providing a connection between the missile and the empennage and acting on the empennage relative to the missile; an attitude detector means for producing a signal proportional to the divergence between the detected and desired attitudes of the missile; an amplifier means for amplifying said signal, said torque transmitter being connected to be driven by the amplified signal produced by said amplifier means; and a source of electrical energy for powering said amplifier and said bi-directional torque transmitter.

Claim 9

A missile according to claim 6, wherein the rotary empennage, includes propulsion means which maintain a predetermined speed of the missile or bring it to said speed.

Claim 10

A missile which includes a system for controlling the attitude of the missile when the missile is moving in a fluid, said system being capable of controlling the attitude of the missile in roll and comprising: a finned rotary empennage concentric with the missile having propulsion means which maintains a predetermined speed of the missile or brings said missile to said speed, said empennage comprises a first jettisonable portion which includes said propulsion means and a first set of foldable fins which can be unfolded upon firing of the missile, and a second non-jettisonable portion which includes a second set of foldable fins, which are held in the folded position by the first jettisonable portion and unfolded when the first portion is jettisoned, thus ensuring that the attitude of the missile can be controlled both before and after the first portion of the empennage is jettisoned; a torque transmitter providing a connection between the missile and the empennage and acting on the empennage relative to the missile; an attitude detector means for producing a signal proportional to the divergence between the detected and desired attitudes of the missile; an amplifier means for amplifying said signal, said torque transmitter being connected to be driven by the amplifier signal produced by said amplifier means.

Claim 11

A missile which includes a system for controlling the attitude of the missile when the missile is moving in a fluid, said system being capable of controlling the attitude of the missile in roll and comprising: a finned rotary empennage concentric with the missile having propulsion means which maintains a predetermined speed of the missile or brings said missile to said speed, said empennage comprises a first jettisonable portion which includes said propulsion means and a first set of foldable fins which can be unfolded upon firing of the missile, and a second non-jettisonable portion which includes a second set of foldable fins, which are held in the folded position by the first jettisonable portion and unfolded when the first portion is jettisoned, thus ensuring that the attitude of the missile can be controlled both before and after the first portion of the empennage is jettisoned; a torque transmitter providing a connection between the missile and the empennage and acting on the empennage relative to the missile; an attitude detector means for producing a signal proportional to the divergence between the detected and desired attitudes of the missile; an amplifier means for amplifying said signal, said torque transmitter being connected to be driven by the amplifier signal produced by said amplifier means.