MEMS inertial navigation systems for aircraft

作者: Y. Dong

DOI: 10.1533/9780857096487.2.177

关键词:

摘要: Abstract: This chapter discusses MEMS accelerometers and gyroscopes how inertial navigation systems (INS) are used with these sensors for aircraft. The first reviews the limitations of to be embedded in INS, then INS integration global positioning (GPS); it provides background on use sensor fusion a Kalman filter aid presents challenges trends

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