The plane of spin acting at right angles to the axis of spin is known as?

Where is the weight of a gyro concentrated to gain higher momentum and therefor stability?

The inertia of mass, keeping the axis rigid or pointing in the same direction is called?

The angular momentum of a given body point remains constant unless some force is applied to change it is called?

The spinning freedom about an axis perpendicular through its centre of spin is?

The tilting freedom about the horizontal axis at right angles to the spin axis of spin is?

The veering freedom about the vertical axis perpendicular to both the spin and tilt axes is the axis of veer

How do we prevent gimbal lock?

What degree are the stops set of max alignment for gimbal lock?

Out of control precession is called?

A gyro having a complete freedom in three planes at right angles to each other, with two gimbals inner tilt and outer veer, is called?

A gyro having freedom in three planes at right angles to each other but controlled by some external force made to point in a desired direction is called?

A tied gyro controlled by gravity to maintain its position relative to the earth , the axis of spin points to the centre of the earth is called?

A tied gyro having one plane of freedom at right angles to the plane of rotation, and one gimbal so constructed as to measure rate of movement about the plane at right angles to both the plane of rotation and the plane of freedom is called?

A unrestricted, unreferenced displacement gyro is called?

Which axis of freedom enables a gyroscopes rotor to spin?

Which axes of freedom does the gyro case or inner gimbal was free to rotate about the horizontal plane, at right angles to the spin axis?

Which axes of freedom does the outer gimbal free to rotate about the vertical plane, which is perpendicular to both the spin and tilt axes and the outer gimbal is supported in the frame or case of the gyro system?

Which gyro has two degrees of freedom it can measure?

What allows the gyro to frame to move around the gyro while it maintains its original attitude and direction of spin axis?

What does not require a gimbal as this plane is simply the freedom of the rotor to spin on its axis?

Increasing the mass of the rotor, concentrating mass neat the rim of the rotor (increasing the radius of gyration) and increasing the rotor speed all increase?

The strength and direction of applied force, moment of inertia of the rotor and angular velocity are all factors which affect the rate of?

The axis which the torque is applied is the?

The axis which precession takes place at is the?

What should older gyros have done to them when aerobatic manoeuvres are to be carried out to avoid damaging the bearings?

What degree of nose up or down from level flight must be avoided to prevent tumbling?

How many degrees an hour would a frictionless space gyro turn from the earth's rotation?

The gyro spin axis being tied horizontal in respect to the indicator case and as such in parallel to the aircraft lateral and longitudinal axes is called?

A vertical gyro that is required to continuously be corrected to the vertical position in relation to the surface of the earth is called a?

DG's, AH's and Bank gyros are all termed?

Which characteristic establishes a stabilised reference unaffected by movement of the supporting body for a reference established gyroscope?

Which characteristic controls the effects of apparent and real drift thus maintaining stabilised reference datums for a reference established gyroscope?

Drift relates to which axis?

If the gyro is not at the equator, what precession value can be used for apparent drift to eliminate the earth rate?

When causing a gyroscope to be processed in the opposite direction to the earths rotation by placing weights in the spin axis of the gyro rotor to unbalance the unit so that the weight force causes the gyro to precess is called?

How is transport rate corrected?

What is a result from imperfections in the manufacture of the gyroscope such as bearing friction or gimbal imbalances and can only be minimised by applying precision engineering techniques called?

Up to what degree of effectiveness is deliberately unbalancing the inner ring to control the earth rate error on a gyro?

What are gimbal errors caused by?

When an aircraft headings such that its longitudinal axis is aligned with the gyro's rotor axis, banking of the aircraft on a constant heading will produce?

Combining a pitch attitude change with an aircraft banking on a constant heading and the longitudinal axis aligned with the gyros rotor axis will cause?

If two pulses of light are sent in opposite direction around a stationary circular loop of radius R, they will travel the same distance at the same speed, so they arrive at the same end point simultaneously is called?

Fibre optic gyros can measure anywhere from?

The longer the path for a fibre optic signal the?

Air driven gyroscope erection systems rely on which characteristic to move the spinning rotor back to a balanced or erect position?

Which air driven gyroscope erection system deflects air evenly across the plate and has no effect on the outer gimbal?

Which type of air driven gyroscope erection system ports the exhausted air through four ports located at right angles to each other to encourage the precession effect to balance it?

Which mechanical gyro erection system uses hooks to capture balls moving around to apply precession force and in the vertical plane the mass of the balls in centred therefore no precession force is applied?

Which mechanical gyro erection system incorporates a slotted disc with a ball free to travel inside the slot and the slot is driven at a uniform speed of 30 rpm?

How is the pitch torque motor positioned in a torque motor?

How is the roll torque motor positioned in a torque motor?

When a gyroscope is in its normal vertical position, where does the mercury lie and which electrode is it in contact with?

What degree will a gyro rotor axis (from the vertical) cause the circuit to the torque motors to interrupt the gimbal system and never erect in a torque motor gyro?

What does the erection rate increase to when the fast erection switch is on?

What duration should you not operate the fast erection switch longer than in case it overheats the stator coils?

When is it appropriate in flight to depress the fast erection switch to prevent false indications of pitch and bank attitude?

When is a permanent magnet used in a DC coil as in case for the correction for apparent drift?

How long does the electromagnet operate for after power has been applied?

How do you correct for erection error in erection systems?

In acceleration, an AH can make a false reading of?

Inclination of gyro spin axis, erection cut out, pitch-bank compensation are all factors which can prevent?

During a turn, the bank levelling switch is disconnected and its erection system is controlled by the pitch levelling switch. What force does the turn need to exceed a 10 degree turn to activate the switch?

Following recovery from unusual attitude, an AH senses gravitational forces, the erection mechanism of caging will immediately begin to correct the precision errors at what rate?

What is the rotor speed of a turn and slip indicator?