Gyro basics Flashcards
2 gyro basic properties
precession
rigidity
factors affecting rigidity
rotational speed
mass
mass distribution
gimbal
frame that allows gyro to maintain orientation and the aircraft to move
space gyro
mounted so it is completely undisturbed by aircraft movements
degrees of freedom
a system with 2 gimbals can rotate in 3 planes without disturbing the gyro, this is quoted as 2 degrees of freedom
1 gimbal 1 degree of freedom
2 gimbal applications
direction indicator
attitude indicator
displacement gyro
used to provide a datum for measuring angular displacement of the aircraft
aircraft displaced not the gyros
space gyros are a type of displacement gyro
wander
have topple(vertical plane) and drift(horizontal plane)
apparent wander: gyro not moving but appears to have moved in relation to observer
earth rotating and transport wander
real wander:
imperfections(random wander) & intentional wander ie from erection systems ,
vert alignment at pole = no wander
apparent drift varies with sine lat
apparent topple varies with cosine lat
precession
gyros response to an unbalanced force
occurs when you apply torque around an axis other than the spin axis
doesn’t move in the direction it is being pushed but as though the force was applied from 90deg further around the gyro
precession opposed by rigidity
rate gyro
1 gimbal
uses precession to measure rates of change
torque applied to an input axis causes gyro to precess
rotates about gimbal (output axis)
used in turn coordinators
gyro power
electric
pneumatic
typical gyro RPMs
few thousand up to 24000RPM
gimbal lock
gyro loses orientation when 2 gimbals become aligned
need to keep gyros 90 deg apart