Optimal Error Dynamics in Missile Guidance
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Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-030-47348-8_2
Reference35 articles.
1. Shima T, Idan M, Golan OM (2006) Sliding-mode control for integrated missile autopilot guidance. J Guid Control Dyn 29(2):250–260
2. Idan M, Shima T, Golan OM (2007) Integrated sliding mode autopilot-guidance for dual-control missiles. J Guid Control Dyn 30(4):1081–1089
3. Dwivedi P, Bhale P, Bhattacharyya A, Padhi R (2016) Generalized estimation and predictive guidance for evasive targets. IEEE Trans Aerosp Electron Syst 52(5):2111–2122
4. He S, Lee C-H (2018) Gravity-turn-assisted optimal guidance law. J Guid Control Dyn 41(1):171–183
5. Kim M, Grider KV (1973) Terminal guidance for impact attitude angle constrained flight trajectories. IEEE Trans Aerosp Electron Syst AES–9(6):852–859
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1. Impact Angle/Time Constraint Guidance Design Based on Fast Terminal Error Dynamics;Journal of Shanghai Jiaotong University (Science);2022-09-24
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