Two Performance Indicators of Reaction Wheel Underactuated Configuration
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-6882-4_1
Reference13 articles.
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2. Hong-xin, W., Shu-ping, T.: Spacecraft control: present and future. Aerospace Cont. Appl. 38(5), 1–7 (2012). https://doi.org/10.3969/j.issn.1674-1579.2012.05.001
3. Xin-sheng, G., Li-qun, C., Yan-zhu, L.: Nonholonomic motion planning for the attitude of rigid spacecraft with two momentum wheel actuators. Control Theory Appl. 21(5), 781–784 (2004). https://doi.org/10.3969/j.issn.1000-8152.2004.05.022
4. Xin-sheng, G., Peng-wei, S.: Nonholonomic motion planning for the attitude of underactuated spacecraft using particle swarm optimization. J. Astronaut. 27(6), 1233–1237 (2006). https://doi.org/10.3321/j.issn:1000-1328.2006.06.022
5. Krishnan, H., Clamroch, N.M., Reyhanoglu, M.: Attitude stabilization of a rigid spacecraft using two momentum wheel actuators. J. Guidance, Cont. Dynam. 18(2), 256–263 (2012). https://doi.org/10.2514/3.21378
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