A Design Method of Missile Acceleration Autopilot Based on Active Disturbance Rejection Control
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[1] William Branch. Autopilot design rules and guidelines , 1998 .
[2] Sheng-De Wang,et al. An adaptive H/sup /spl infin// controller design for bank-to-turn missiles using ridge Gaussian neural networks , 2004, IEEE Transactions on Neural Networks.
[3] Zhiqiang Gao,et al. Scaling and bandwidth-parameterization based controller tuning , 2003, Proceedings of the 2003 American Control Conference, 2003..
[4] H. Buschek. FULL ENVELOPE MISSILE AUTOPILOT DESIGN USING GAIN SCHEDULED ROBUST CONTROL , 1999 .
[5] C. F. Lin,et al. Application of Sliding Mode Control to Bank-To-Turn Missile Systems , 1993, Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,.
[6] Bor-Sen Chen,et al. Robust adaptive optimal tracking design for uncertain missile systems: a fuzzy approach , 2002, Fuzzy Sets Syst..