Normal gravity model for inertial navigation of a hypersonic boost-glide vehicle
Author:
Publisher
Zhejiang University Press
Subject
General Engineering
Link
https://link.springer.com/content/pdf/10.1631/jzus.A2100133.pdf
Reference23 articles.
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2. Becka S, Novack M, Slivinsky S, et al., 2008. A high reliability solid state accelerometer for ballistic missile inertial guidance. Proceedings of AIAA Guidance, Navigation and Control Conference and Exhibit, p.7300. https://doi.org/10.2514/6.2008-7300
3. Bykerk T, Verstraete D, Steelant J, 2020. Low speed longitudinal aerodynamic, static stability and performance analysis of a hypersonic waverider. Aerospace Science and Technology, 96:105531. https://doi.org/10.1016/j.ast.2019.105531
4. Chachan Y, Stevenson DJ, 2019. A linear approximation for the effect of cylindrical differential rotation on gravitational moments: application to the non-unique interpretation of Saturn’s gravity. ICARUS, 323:87–98. https://doi.org/10.1016/j.icarus.2018.12.020
5. Chang LB, Qin FJ, Wu MP, 2019. Gravity disturbance compensation for inertial navigation system. IEEE Transactions on Instrumentation and Measurement, 68(10):3751–3765. https://doi.org/10.1109/TIM.2018.2879145
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