Robust Helicopter Sliding Mode Control for Enhanced Handling and Trajectory Following

[1]  Christopher Edwards,et al.  Robust model reference control using a sliding mode controller/observer scheme with application to a helicopter problem , 1996, Proceedings. 1996 IEEE International Workshop on Variable Structure Systems. - VSS'96 -.

[2]  Marc T. Höfinger,et al.  Impact of turbulence and degraded visual environment on pilot workload , 2017 .

[3]  Joseph F. Horn,et al.  Simulation Testing of Advanced Response Types for Ship-Based Rotorcraft , 2014 .

[4]  Ian Postlethwaite,et al.  H∞ Control of the NRC Bell 205 Fly-by-Wire Helicopter , 1999 .

[5]  A. J. Fossard Helicopter control law based on sliding mode with model following , 1993 .

[6]  Michael Jump,et al.  Handling Qualities Requirements for Future Personal Aerial Vehicles , 2013 .

[7]  Christopher Edwards,et al.  Sliding mode control : theory and applications , 1998 .

[8]  Yuri B. Shtessel,et al.  Reusable Launch Vehicle Control in Multiple Time Scale Sliding Modes , 2000 .

[9]  Carl J. Ockier Flight Evaluation of the New Handling Qualities Criteria Using the BO 105. , 1996 .

[10]  Ranjan Ganguli,et al.  Neural network based feedback error controller for helicopter , 2011 .

[11]  Matthew S. Whalley,et al.  Optimization of Partial Authority Automatic Flight Control Systems for Hover/Low-Speed Maneuvering in Degraded Visual Environments , 1999 .

[12]  Ian Postlethwaite,et al.  Evaluating H∞ controllers on the NRC Bell 205 fly-by-wire helicopter , 1999 .

[13]  Mark B. Tischler,et al.  Modernized Control Laws for UH-60 BLACK HAWK Optimization and Flight-Test Results , 2005 .

[14]  I. Postlethwaite,et al.  Static I loop shaping control of a fly-by-wire helicopter , 2005, Autom..

[15]  Joost Venrooij,et al.  Transforming Civil Helicopters into Personal Aerial Vehicles: Modeling, Control, and Validation , 2017 .

[16]  David McGeoch,et al.  MIMO Sliding Mode Attitude Command Flight Control System For a Helicopter , 2005 .

[17]  Manfred Hajek,et al.  Requirements and Design Challenges in Rotorcraft Flight Simulations for Research Applications , 2015 .

[18]  Yuri B. Shtessel,et al.  Multiple Timescale Flight Control Using Reconfigurable Sliding Modes , 1999 .

[19]  S. Seher-Weiss,et al.  Development of EC 135 turbulence models via system identification , 2012 .

[20]  Pedro Simplício,et al.  An acceleration measurements-based approach for helicopter nonlinear flight control using Incremental Nonlinear Dynamic Inversion , 2013 .

[21]  T Clarke,et al.  Desirable eigenstructure for good short-term helicopter handling qualities: The attitude command response case , 2003 .

[22]  Eicher Low,et al.  Design of Attitude and Rate Command Systems for Helicopters Using Eigenstructure Assignment , 1989 .

[23]  Peter G. Hamel,et al.  Advances in rotorcraft system identification , 1997 .

[24]  Eric N. Johnson,et al.  Adaptive Flight Control for an Autonomous Unmanned Helicopter , 2002 .

[25]  Chris L. Blanken,et al.  Empirically Derived Helicopter Response Model and Control System Requirements for Flight in Turbulence , 2004 .

[26]  John Y. Hung,et al.  Variable structure control: a survey , 1993, IEEE Trans. Ind. Electron..