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Analytical study of a technique for the elimination of steering rate gyro bias in a typical missile autopilot

机译：典型导弹自动驾驶仪中消除操舵率陀螺偏向技术的分析研究

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Digitized by Kansas State University Libraries

机译：堪萨斯州立大学图书馆数字化

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Eslinger Robert Clayton;
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年度 2011
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正文语种 en_US
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2. APPLICATION OF REAL/MIXED MU COMPUTATIONAL TECHNIQUES TO AN H(INFINITY) MISSILE AUTOPILOT [J] . Ferreres G., Duc G., Msaad M., International Journal of Robust and Nonlinear Control . 1996,第8期

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3. Practical method for eliminating the magnetic bias sensitivity of square ring laser gyros by adjusting the nonplanar angle [J] . Meixiong Chen, Jie Yuan, Zhiguo Wang, Optics Communications: A Journal Devoted to the Rapid Publication of Short Contributions in the Field of Optics and Interaction of Light with Matter . 2014,第Null期

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4. Analytical guidance laws and integrated guidance/autopilot for homing missiles [C] . Balakrishnan, S.N., Stansbery, . 1993

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6. An Innovative Strategy for Accurate Thermal Compensation of Gyro Bias in Inertial Units by Exploiting a Novel Augmented Kalman Filter [O] . Rita Fontanella, Domenico Accardo, Rosario Schiano Lo Moriello, 2018

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Analytical study of a technique for the elimination of steering rate gyro bias in a typical missile autopilot

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