Inertial Navigation | AHRS Flashcards
AHRS stands for ____
Altitude and Heading Reference System
AHRS replaces ____ ___ and their problems
traditional gyros
The problems which AHRS aims to eliminate include:
- Drift
- Topple
- Gimbal lock
AHRS is generally installed in aircraft which do not had a ___
IRS
AHRS consists of a group of inertial sensors in one package that can output ___, ___, and ___ information to flight deck displays.
attitude, heading, and glitch dynamics
A ___ valve and ADC are involved.
flux
3D orientation is obtained by integrating the gyroscopes with ___ and ___
accelerometers, megneotmeters
AHRS requires ___ power, ___ wiring, weighs ___, and has a ___ footprint.
less less less smaller
Micro Electro Mechanical System gyroscopes have __ power requirements and costs by using ___ ___ to measure the angular rate
low Coriolis Effect
Most use a ___ fork assembly
tuning
With the tuning fork configuration, two masses oscillate and move constantly in ___ directions
opposite
During linear acceleration, two masses move in the ___ direction, meaning no change in capacitance will be detected
same
When angular velocity is applied, the coriolis force on each mass produces a change in ___ that is proportional to the angular velocity, which is then converted into output voltage.
capacitance
The magnetometer will usually be mounted remotely from the AHRS, where magentic disturbances are ___
minimal
Three different types of MEMS exist:
- Accelerometers
- Rate Gyros
- Magnetometers