Author:
Hwang Donghyeok,Tahk Min-Jea
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering
Reference18 articles.
1. Abd-elatif MA, Qian L, Bo Y (2016) Optimization of three-loop missile autopilot gain under crossover frequency constraint. Def Technol 12:32–38
2. Mracek CP, Ridgely DB (2005) Missile longitudinal autopilots: connections between optimal control and classical topologies. AIAA guidance, navigation, and control conference, San Francisco
3. Mracek CP, Ridgely DB (2005) Missile longitudinal autopilots: comparison of multiple three loop topologies. AIAA guidance, navigation, and control conference, San Francisco
4. Xu H, Mirmirani MD, Ioannou PA (2004) Adaptive sliding mode control design for a hypersonic flight vehicle. J Guidance Control Dyn 27(5):829–839
5. Lee Y, Kim Y, Moon G, Jun BE (2014) Boost phase missile attitude controller design using higher-order sliding modes. 29th Congress of the international council of the aeronautical sciences (ICAS 2014), Curran Associates, Inc., Red Hook, NY, pp 3237–3244
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