An Adaptive RISE-Based Guidance Method with Impact Angle Constraint
Author:
Publisher
Springer Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-15-8155-7_229
Reference8 articles.
1. Wang, X., Zhang, Y., Wu, H.: Distributed cooperative guidance of multiple anti-ship missiles with arbitrary impact angle constraint. Aerosp. Sci. Technol. 46, 299–311 (2015)
2. Zhang, Z., Li, S., Luo, S.: Terminal guidance laws of missile based on ISMC and NDOB with impact angle constraint. Aerosp. Sci. Technol. 31(1), 30–41 (2013)
3. Sharma, Y.R., Ratnoo, A.: A bearings-only trajectory shaping guidance law with look-angle constraint. IEEE Trans. Aerosp. Electron. Syst. 55(6), 3303–3315 (2019)
4. Lee, C.-H., Kim, T.-H., Tahk, M.-J.: Interception Angle control guidance using proportional navigation with error feedback. J. Guid. Control Dyn. 36(5), 1556–1561 (2013)
5. Xian, B., Dawson, D.M., Queiroz, M.S.D., Chen, J.: A continuous asymptotic tracking control strategy for uncertain nonlinear systems. IEEE Trans. Autom. Control 49(7), 1206–1211 (2004)
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