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1. Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft
by Parrish, Russell V and Williams, Steven P and Langley Research Center
1990, 59
Rotorcraft | Hovering | Flight simulation
Book
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2. The application of CFD to rotary wing flow problems
by Caradonna, Francis X and Ames Research Center
1992, 72
Computational fluid dynamics | Rotorcraft | Rotordynamics
Book
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3. The effects of tailwinds and control cross coupling on rotorcraft handling qualities for steep, decelerating instrument approaches and missed approaches
by Baillie, S. W and Kereliuk, S and Morgan, J. M and National Research Council Canada. Institute for Aerospace Research
1993, Aeronautical note, Volume IAR-AN-77, 67
Handling qualities | Rotorcraft aircraft | Instrument approach
Book
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4. Full Text Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings – A design perspective
by Pavel, Marilena D and Masarati, Pierangelo and Gennaretti, Massimo and Jump, Michael and Zaichik, Larisa and Dang-Vu, Binh and Lu, Linghai and Yilmaz, Deniz and Quaranta, Giuseppe and Ionita, Achim and Serafini, Jacopo
Progress in Aerospace Sciences, ISSN 0376-0421, 07/2015, Volume 76, pp. 55 - 89
Understanding, predicting and supressing the inadvertent aircraft oscillations caused by Aircraft/Rotorcraft Pilot Couplings (A/RPC) is a challenging problem... 
Aircraft-Pilot Couplings (APC) | Preliminary design | Flight control system design | Rotorcraft-Pilot Coupling (RPC) | Conceptual design | Automatic flight control system (AFCS) | Pilot induced oscillations (PIO) | Pilot assisted oscillations (PAO) | Automatic flight controlsystem(AFCS) | Pilot assistedoscillations(PAO) | Flight controlsystemdesign | Pilot inducedoscillations(PIO) | Rotorcraft-PilotCoupling(RPC) | Aircraft-Pilot Couplings(APC) | QUALITIES | INFORMATION | ENGINEERING, AEROSPACE | FLIGHT | MODELS | OPTIMIZATION | TECHNOLOGY | Couplings | Aircraft components | Biodynamics | Pilots | Control systems | Rotorcraft | Modelling | Aircraft
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5. Eigenstructure control algorithms
: applications to aircraft/ rotorcraft handling qualities design
by Srinathkumar, S
2011, IET control engineering series, ISBN 1849192596, Volume 74., xv, 285
This book demonstrates that eigenstructure control theory can be easily adapted and infused into aircraft industry's stringent design practices. Thus... 
Automatic pilot (Airplanes) | Flight control | Flight Control., Automatic Pilot (Airplanes) | Eigenvalues
Book
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6. Full Text Effect of turbulence modeling for the prediction of flow and heat transfer in rotorcraft avionics bay
by Akin, Altug and Kahveci, Harika S
Aerospace Science and Technology, ISSN 1270-9638, 12/2019, Volume 95, p. 105453
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7. Full Text The role of rotor coning in helicopter proneness to collective bounce
by Muscarello, Vincenzo and Quaranta, Giuseppe and Masarati, Pierangelo
Aerospace Science and Technology, ISSN 1270-9638, 07/2014, Volume 36, pp. 103 - 113
Collective bounce is a rotorcraft–pilot coupling phenomenon caused by vertical vibrations in the aircraft cockpit that are transmitted to the collective lever... 
Collective bounce | Biodynamic feedthrough | Rotorcraft–pilot couplings | Rotorcraft-pilot couplings | ENGINEERING, AEROSPACE | Helicopters | Analysis
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8. Full Text Design and aeromechanics investigation of compound helicopters
by Yeo, Hyeonsoo
Aerospace Science and Technology, ISSN 1270-9638, 05/2019, Volume 88, pp. 158 - 173
This paper reviews lessons learned from the compound helicopter studies performed by NASA and the US Army Aviation Development Directorate to support the NASA... 
Comprehensive analysis | Rotorcraft design | Compound helicopter | Rotorcraft aeromechanics analysis | SYSTEM | ENGINEERING, AEROSPACE | Military helicopters | Aerodynamics | Analysis | Investigations
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9. Development of a 3D CFD aerodynamic optimization tool and application to engine air intake design
by Millot, Grégory and Scholz, Olivier and Ouhamou, Saïd and Becquet, Mathieu and Magnabal, Sébastien
International Journal of Numerical Methods for Heat and Fluid Flow, ISSN 0961-5539, 2019
CFD | Rotorcraft | Engine air intake | Optimization
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10. New method of aeromagnetic surveys with rotorcraft UAV in particular areas
by Li, Zhipeng and Gao, Song and Wang, Xuben
Acta Geophysica Sinica, ISSN 0001-5733, 09/2018, Volume 61, Issue 9, pp. 3825 - 3834
Fluxgate | Rotorcraft UAV | Particular area | Aeromagnetic survey
Journal Article
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11. Full Text Practises to identify and prevent adverse aircraft-and-rotorcraft-pilot couplings—A ground simulator perspective
by Pavel, Marilena D and Jump, Michael and Masarati, Pierangelo and Zaichik, Larisa and Dang-Vu, Binh and Smaili, Hafid and Quaranta, Giuseppe and Stroosma, Olaf and Yilmaz, Deniz and Johnes, Michael and Gennaretti, Massimmo and Ionita, Achim
Progress in Aerospace Sciences, ISSN 0376-0421, 08/2015, Volume 77, pp. 54 - 87
The aviation community relies heavily on flight simulators as a fundamental tool for research, pilot training and development of any new aircraft design. The... 
Simulator Fidelity | Motion Cues | APC | Visual Cues | Aircraft Pilot Couplings | Pilot Induced Oscillations (PIO) | Biodynamic Feedthrough | Control Loading | Rotorcraft Pilot Couplings (RPC) | Time delay | Pilot Assisted Oscillations (PAO) | Latency | Rotorcraft (RPC) | Aircraft Pilot Couplings (APC) | ENGINEERING, AEROSPACE | Aeronautics | Aviation | Simulation | Flight simulators | Tools | Grounds | Assessments | Aircraft | Pilot training
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12. Full Text RUAV System Identification and Verification Using A Frequency-Domain Methodology
by Viguria, A and Heredia, Guillermo and Ollero, Aníbal and Santamaría, D and Sánchez, I
2014, ISBN 9783319034126, Volume 252, 19
Aircraft modelling and control | Rotorcraft | Identification | UAV | UAV modelling and control | CIFER
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13. Full Text The Triangular Quadrotor: A More Efficient Quadrotor Configuration
by Driessens, Scott and Pounds, Paul
IEEE Transactions on Robotics, ISSN 1552-3098, 12/2015, Volume 31, Issue 6, pp. 1517 - 1526
We describe a new configuration of fixed-pitch miniature robot rotorcraft that combines the energetic efficiency of a helicopter and the mechanical simplicity... 
Torque | multirotors | Helicopters | Rotors | Unmanned aerial vehicles | rotorcraft | PD control | Aerial robotics | ROBOTICS | Research | Analysis
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14. Full Text The dynamic analysis of a cracked Timoshenko beam by the spectral element method
by Krawczuk, M and Palacz, M and Ostachowicz, W
Journal of Sound and Vibration, ISSN 0022-460X, 2003, Volume 264, Issue 5, pp. 1139 - 1153
The aim of this paper is to introduce a new finite spectral element of a cracked Timoshenko beam for modal and elastic wave propagation analysis. The proposed... 
ACOUSTICS | ROTORCRAFT FLEXBEAMS | MECHANICS | DAMAGE | ENGINEERING, MECHANICAL
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15. Full Text Non-Linear Dynamic Inversion Control Design for Rotorcraft
by Horn, Joseph
Aerospace, ISSN 2226-4310, 03/2019, Volume 6, Issue 3, p. 38
Flight control design for rotorcraft is challenging due to high-order dynamics, cross-coupling effects, and inherent instability of the flight dynamics.... 
rotorcraft handling qualities | dynamic inversion | rotorcraft flight control
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16. Full Text Autonomous landing at unprepared sites by a full-scale helicopter
by Scherer, Sebastian and Chamberlain, Lyle and Singh, Sanjiv
Robotics and Autonomous Systems, ISSN 0921-8890, 12/2012, Volume 60, Issue 12, pp. 1545 - 1562
Helicopters are valuable since they can land at unprepared sites; however, current unmanned helicopters are unable to select or validate landing zones (LZs)... 
Lidar | Landing zone selection | Rotorcraft | UAV | 3D perception | ROBOTICS | TERRAIN | UNMANNED ROTORCRAFT | AUTOMATION & CONTROL SYSTEMS | COMPUTER SCIENCE, ARTIFICIAL INTELLIGENCE | Robots | Algorithms | Clouds | Helicopters | Terrain | Grounds | Perception | Landing | Autonomous | Land
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17. Full Text Robust Backstepping Sliding-Mode Control and Observer-Based Fault Estimation for a Quadrotor UAV
by Fuyang Chen and Rongqiang Jiang and Kangkang Zhang and Bin Jiang and Gang Tao
IEEE Transactions on Industrial Electronics, ISSN 0278-0046, 08/2016, Volume 63, Issue 8, pp. 5044 - 5056
This study gives the mathematic model of a quadrotor unmanned aerial vehicle (UAV) and then proposes a robust nonlinear controller which combines the... 
Backstepping control | unmanned aerial vehicle (UAV) | Backstepping | Attitude control | Rotors | Estimation | sliding-mode control (SMC) | Robustness | Mathematical model | fault estimation | robustness | LINEARIZATION | AIRCRAFT | DESIGN | VEHICLE | STABILIZATION | ATTITUDE-CONTROL | DRIVEN | DISTURBANCE OBSERVER | ENGINEERING, ELECTRICAL & ELECTRONIC | INSTRUMENTS & INSTRUMENTATION | SYSTEMS | HELICOPTER | AUTOMATION & CONTROL SYSTEMS | Usage | Mathematical models | Research | Helicopters | Unmanned aerial vehicles | Controllers | Faults | Computer simulation | Rotorcraft | Nonlinearity | Sliding mode control
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18. Car-like steering concepts for rotorcraft
by Schuchardt, Bianca Isabella
DLR Deutsches Zentrum fur Luft- und Raumfahrt e.V. - Forschungsberichte, ISSN 1434-8454, 2017, Volume 2017-, Issue 65, pp. 1 - 194
Control | Helicopter | Steering wheel | Rotorcraft
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19. Full Text Numerical investigation of the aerodynamic interaction between a tiltrotor and a tandem rotor during shipboard operations
by Tan, Jian Feng and Zhou, Tian Yi and Sun, Yi Ming and Barakos, George N
Aerospace Science and Technology, ISSN 1270-9638, 04/2019, Volume 87, pp. 62 - 72
Complex rotorcraft-to-rotorcraft interference problems occur during shipboard operations, and have a negative impact on safety. A vortex-based approach is used... 
Viscous boundary model | Rotorcraft-to-rotorcraft interference | Vortex particle method | Flow field | Shipboard operation | CONVECTION-DIFFUSION EQUATIONS | VORTEX PARTICLE | ENGINEERING, AEROSPACE | SIMULATION | WEIGHTED PARTICLE METHOD | HELICOPTER FUSELAGE | BLUFF-BODY FLOWS | DYNAMICS
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20. Full Text Adaptive trajectory tracking control of output constrained multi-rotors systems
by Zuo, Zongyu and Wang, Chenliang
IET Control Theory and Applications, ISSN 1751-8644, 9/2014, Volume 8, Issue 13, pp. 1163 - 1174
The design of output constrained control system for unmanned aerial vehicles deployed in confined areas is an important issue in practice and not taken into... 
COMMAND-FILTERED COMPENSATION | NEURAL-CONTROL | ROTORCRAFT | INSTRUMENTS & INSTRUMENTATION | NONLINEAR-SYSTEMS | CONTROL DESIGN | STABILIZATION | FLIGHT CONTROL | QUADROTOR HELICOPTER | UAV | AUTOMATION & CONTROL SYSTEMS | ENGINEERING, ELECTRICAL & ELECTRONIC
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