Variable Structure Control Based Flight Control Systems For Aircraft And Missiles
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Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors
Das, Priya G (2011-03-17)To address the concern of classical guidance and control designs (where guidance and control loops are designed separately in an “outer loop – inner loop” structure), integrated guidance and control (IGC) ideas have been ... -
Decoupled Lateral Directional Flight Control System Design Using Eigenstructure Assignment Method
Dixit, Girish G (2012-11-07) -
Sliding Mode Control Based Guidance Strategies with Terminal Constraints
Kumar, Shashi Ranjan (2018-07-23)In the guidance literature, minimizing miss distance along with optimizing the energy usage had been an objective for several decades. In current day applications, additional terminal performance such as impact angle and ...