Three-Dimensional Sliding Mode Guidance Law Based on Variable Universe Fuzzy Control
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-6613-2_574
Reference12 articles.
1. Viswanath, D., Deb, D.: Disturbance observer based sliding mode control for proportional navigation guidance. In: IFAC Workshop on Embedded Guidance, Navigation and Control in Aerospace 2012: Bangalore, India, 13–15 February 2012, pp. 163–168. Curran Associates, Inc. (2012)
2. Guo, G.: Application of variable universe strategy in missile fuzzy guidance law design. Firepower Command Control 36(5), 177–180 (2011). https://doi.org/10.3969/j.issn.1002-0640.2011.05.048
3. Wang, Q., Bi, J.: Design and simulation of a fuzzy terminal guidance law robust to noise interference. J. Syst. Simul. 16(1), 137–139 (2004). https://doi.org/10.3969/j.issn.1004-731X.2004.01.039
4. Siyu, H., Xugang, W., Yin, Z.: Sliding-mode control for a rolling-missile input constraints. Syst. Eng. Electron. Technol. (English Version) 31(5), 1041–1050 (2020). https://doi.org/10.23919/JSEE.2020.00007
5. Fixed-time adaptive model reference sliding mode control for an air-to-ground missile. Chinese J. Aviation (English Version) 32(5), 1268–1280 (2019)
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