The additional error emergence of inertial sensors in the operational conditions of hypersonic flight
Author:
Affiliation:
1. Łukasiewicz Research Network – Industrial Research Institute for Automation and Measurements PIAP,Warsaw,Poland
2. National Technical University of Ukraine "IGOR SIKORSKY KYIV POLYTECHNIC INSTITUTE",Kyiv,Ukraine
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10019601/10019606/10019695.pdf?arnumber=10019695
Reference12 articles.
1. Optimization design of Angle sensor for three-float gyro based on finite element analysis method;wu;Zhongguo Guanxing Jishu Xuebao/journal of Chinese Inertial Technology,2021
2. Sound transmission loss of an inertant metamaterial plate submerged in moving fluids
3. Investigation of optimization of combustion processes in the engine of combat vehicles by use of disk structure;korobiichuk;Energies,2021
4. Effect of Acoustic Shock on Submarine
5. The Additional Error of Inertial Sensors Induced by Hypersonic Flight Conditions
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