Satellite Radio Navigation and Inertial Navigation MCQs

Welcome to our comprehensive collection of Multiple Choice Questions (MCQs) on Satellite Radio Navigation and Inertial Navigation, a fundamental topic in the field of Avionics Engineering. Whether you're preparing for competitive exams, honing your problem-solving skills, or simply looking to enhance your abilities in this field, our Satellite Radio Navigation and Inertial Navigation MCQs are designed to help you grasp the core concepts and excel in solving problems.

In this section, you'll find a wide range of Satellite Radio Navigation and Inertial Navigation mcq questions that explore various aspects of Satellite Radio Navigation and Inertial Navigation problems. Each MCQ is crafted to challenge your understanding of Satellite Radio Navigation and Inertial Navigation principles, enabling you to refine your problem-solving techniques. Whether you're a student aiming to ace Avionics Engineering tests, a job seeker preparing for interviews, or someone simply interested in sharpening their skills, our Satellite Radio Navigation and Inertial Navigation MCQs are your pathway to success in mastering this essential Avionics Engineering topic.

Note: Each of the following question comes with multiple answer choices. Select the most appropriate option and test your understanding of Satellite Radio Navigation and Inertial Navigation. You can click on an option to test your knowledge before viewing the solution for a MCQ. Happy learning!

So, are you ready to put your Satellite Radio Navigation and Inertial Navigation knowledge to the test? Let's get started with our carefully curated MCQs!

Satellite Radio Navigation and Inertial Navigation MCQs | Page 5 of 9

Q41.
In flexure pivot accelerometer, the torque current is a measure of acceleration.
Discuss
Answer: (a).True
Q42.
Why do accelerometers that include fluid damping exhibit reduced damping?
Discuss
Answer: (d).Thermal characters
Q43.
An accelerometer can only measure acceleration in one direction?
Discuss
Answer: (a).True
Discuss
Answer: (a).Flexure must provide maximum resistance in the direction of input axis
Q45.
Which of the following conditions cause rectification of vibration inputs?
Discuss
Answer: (a).Heating
Q46.
What does silicon accelerometers use for proof mass sensing and for rebalancing?
Discuss
Answer: (c).Metalised wafers
Q47.
Which type of rebalancing technique use voltage applied to pendulum and electrode for correction?
Discuss
Answer: (b).Voltage forcing
Q48.
What is the purpose of a gyro in an inertial navigation system?
Discuss
Answer: (a).Space-stabilize the accelerometer
Q49.
What is the range of an order of angular rate magnitude that gyros used in military planes need?
Discuss
Answer: (b).8.5
Q50.
Why are unfloated instruments with ball bearings not suitable for air navigation?
Discuss
Answer: (b).High drift rate
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