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書(shū)目名稱Gyro-Free Inertial Navigation Technology影響因子(影響力)




書(shū)目名稱Gyro-Free Inertial Navigation Technology影響因子(影響力)學(xué)科排名




書(shū)目名稱Gyro-Free Inertial Navigation Technology網(wǎng)絡(luò)公開(kāi)度




書(shū)目名稱Gyro-Free Inertial Navigation Technology網(wǎng)絡(luò)公開(kāi)度學(xué)科排名




書(shū)目名稱Gyro-Free Inertial Navigation Technology被引頻次




書(shū)目名稱Gyro-Free Inertial Navigation Technology被引頻次學(xué)科排名




書(shū)目名稱Gyro-Free Inertial Navigation Technology年度引用




書(shū)目名稱Gyro-Free Inertial Navigation Technology年度引用學(xué)科排名




書(shū)目名稱Gyro-Free Inertial Navigation Technology讀者反饋




書(shū)目名稱Gyro-Free Inertial Navigation Technology讀者反饋學(xué)科排名

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Dri727

Attitude Resolution of GFINS,fficult for GFINS to achieve the angular velocity resolution accuracy of SINS; thus, it is very important to improve the attitude resolution algorithm accuracy for GFINS. Quarternion based attitude resolution algorithm for GFINS is presented in Chap.?..

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強(qiáng)制性

Elias T. Ayuk,Samuel Tambi KaboréS measure a vehicle’s linear motion and angular motion by gyroscopes and accelerometers, and then resolves the vehicle’s attitude and position. The primary inertial units of the INS include the gyroscope and accelerometer. The gyroscope is used to measure the vehicle’s angular motion, and the accele

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https://doi.org/10.1007/978-3-662-63129-4 a prerequisite and one of the key factors affecting the INS accuracy. Initial alignment is a process to establish initial conditions for the INS; it is one of the key technologies necessary to realize inertial navigation. GFINS self-dependent alignment technology and external information-aided alig

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