Tilt-Wing eVTOL Takeoff Trajectory Optimization
暂无分享,去创建一个
[1] J. Young,et al. Propeller at high incidence , 1965 .
[2] Mark D. Maughmer,et al. Relaxed-Wake Vortex-Lattice Method Using Distributed Vorticity Elements , 2008 .
[3] Roland Siegwart,et al. Model-based transition optimization for a VTOL tailsitter , 2017, 2017 IEEE International Conference on Robotics and Automation (ICRA).
[4] R. H. Stone,et al. Aerodynamic Modeling of the Wing-Propeller Interaction for a Tail-Sitter Unmanned Air Vehicle , 2008 .
[5] J. Gordon Leishman,et al. Principles of Helicopter Aerodynamics , 2000 .
[6] Colin R. Theodore,et al. Greased Lightning (GL-10) Flight Testing Campaign , 2017 .
[7] Daisuke Kubo,et al. Tail-Sitter Vertical Takeoff and Landing Unmanned Aerial Vehicle: Transitional Flight Analysis , 2008 .
[8] H. L. Kelley,et al. Summary of a flight-test evaluation of the CL-84 tilt-wing V/STOL aircraft , 1970 .
[9] C. P. van Dam,et al. Design-oriented high-lift methodology for general aviation and civil transport aircraft , 2001 .
[10] R. Mukherjee,et al. Poststall prediction of multiple-lifting-surface configurations using a decambering approach , 2004 .
[11] Michael S. Selig,et al. Real-Time Flight Simulation of Highly Maneuverable Unmanned Aerial Vehicles , 2014 .
[12] Joaquim R. R. A. Martins,et al. A Computational Architecture for Coupling Heterogeneous Numerical Models and Computing Coupled Derivatives , 2018, ACM Trans. Math. Softw..
[13] Joaquim R. R. A. Martins,et al. An adaptive approach to constraint aggregation using adjoint sensitivity analysis , 2007 .
[14] Masayuki Sato,et al. Flight Controller Design and Demonstration of Quad-Tilt-Wing Unmanned Aerial Vehicle , 2015 .
[15] Graeme J. Kennedy,et al. An evaluation of constraint aggregation strategies for wing box mass minimization , 2017 .
[16] A. Strauß. Theory Of Wing Sections Including A Summary Of Airfoil Data , 2016 .
[17] Dieter Moormann,et al. Unified Velocity Control and Flight State Transition of Unmanned Tilt-Wing Aircraft , 2017 .
[18] Sally A. Viken,et al. Comparison of High-Fidelity Computational Tools for Wing Design of a Distributed Electric Propulsion Aircraft , 2017 .
[19] Tomas Sinnige,et al. Validation and Comparison of RANS Propeller Modeling Methods for Tip-Mounted Applications , 2018, AIAA Journal.
[20] L. A. Viterna,et al. Fixed pitch rotor performance of large horizontal axis wind turbines , 1982 .
[21] Peter W. Gibbens,et al. Flight Testing of the T-Wing Tail-Sitter Unmanned Air Vehicle , 2008 .
[22] Mark D. Maughmer,et al. Higher-Order Free-Wake Method for Propeller–Wing Systems , 2019, Journal of Aircraft.
[23] Charles R. Hargraves. AN ANALYTICAL STUDY OF THE LONGITUDINAL DYNAMICS OF A TILT-WING VTOL , 1961 .
[24] Tobias Ostermann,et al. Design and wind tunnel tests of a tiltwing UAV , 2011 .
[25] J. Konrad. Flight and operational suitability testing of the XC-142, V/STOL assault transport , 1967 .
[26] L. Prandtl. Induced drag of multiplanes , 1924 .
[27] Eric Laurendeau,et al. VLM Coupled with 2.5D RANS Sectional Data for High-Lift Design , 2018 .
[28] Peng Wei,et al. Energy Optimal Speed Profile for Arrival of Tandem Tilt-Wing eVTOL Aircraft with RTA Constraint , 2018, 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC).
[29] Brian J. German,et al. A surrogate-based multi-disciplinary design optimization framework modeling wing–propeller interaction , 2018, Aerospace Science and Technology.
[30] Mahmut Faruk Aksit,et al. Design and construction of a novel quad tilt-wing UAV , 2012 .
[31] H. Glauert. A GENERAL THEORY OF THE AUTOGYRO , 2022 .
[32] C. Hargraves,et al. DIRECT TRAJECTORY OPTIMIZATION USING NONLINEAR PROGRAMMING AND COLLOCATION , 1987 .
[33] Wayne Johnson,et al. Concept Vehicles for VTOL Air Taxi Operations , 2018 .
[34] Nicholas K. Borer,et al. High-Lift Propeller System Configuration Selection for NASA's SCEPTOR Distributed Electric Propulsion Flight Demonstrator , 2016 .
[35] Nicholas K. Borer,et al. Drag Reduction Through Distributed Electric Propulsion , 2014 .
[36] Robert D. Falck,et al. Simultaneous Propulsion System and Trajectory Optimization , 2017 .
[37] J Pegg Robert,et al. Summary of Flight-Test Results of the VZ-2 Tilt-Wing Aircraft , 1962 .
[38] G. Kreisselmeier,et al. SYSTEMATIC CONTROL DESIGN BY OPTIMIZING A VECTOR PERFORMANCE INDEX , 1979 .
[39] Michael A. Saunders,et al. SNOPT: An SQP Algorithm for Large-Scale Constrained Optimization , 2002, SIAM J. Optim..
[40] Atsushi Konno,et al. Optimal transition from hovering to level-flight of a quadrotor tail-sitter UAV , 2017, Auton. Robots.
[41] Richard E Kuhn,et al. Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 degrees , 1956 .
[42] J. L. Tangler,et al. Horizontal axis wind turbine post stall airfoil characteristics synthesization , 1991 .
[43] Inderjit Chopra,et al. Basic Understanding of Airfoil Characteristics at Low Reynolds Numbers (104–105) , 2017 .
[44] J. R. Chambers,et al. Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests , 1968 .
[45] John T. Hwang,et al. Large-Scale Multidisciplinary Optimization of an Electric Aircraft for On-Demand Mobility , 2018 .
[46] C. P. van Dam,et al. The aerodynamic design of multi-element high-lift systems for transport airplanes , 2002 .
[47] Ashok Gopalarathnam,et al. A CFD Database for Airfoils and Wings at Post-Stall Angles of Attack , 2013 .
[48] H. H. Heyson,et al. Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 degrees to 180 degrees , 1955 .
[49] Brian J. German,et al. Conceptual Design of Electric Aircraft with Distributed Propellers: Multidisciplinary Analysis Needs and Aerodynamic Modeling Development , 2014 .
[50] C. B. Fay,et al. A CURSORY ANALYSIS OF THE VTOL TILT‐WING PERFORMANCE AND CONTROL PROBLEMS , 1963 .
[51] Michael Dobson Patterson,et al. Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft , 2016 .
[52] Tiauw Hiong Go,et al. Optimization of transition maneuvers through aerodynamic vectoring , 2012 .
[53] Joaquim R. R. A. Martins,et al. OpenMDAO: an open-source framework for multidisciplinary design, analysis, and optimization , 2019, Structural and Multidisciplinary Optimization.
[55] J W Gebhard,et al. ACCELERATION AND COMFORT IN PUBLIC GROUND TRANSPORTATION , 1970 .
[56] J. Nichols. The Hiller X-18 experimental aircraft - Lessons learned , 1990 .
[57] Michael S. Selig,et al. Modeling full-envelope aerodynamics of small UAVs in realtime , 2010 .
[58] Joaquim R. R. A. Martins,et al. The complex-step derivative approximation , 2003, TOMS.
[59] R. H. Kirby,et al. AERODYNAMIC FACTORS TO BE CONSIDERED IN THE DESIGN OF TILT‐WING V/STOL AIRPLANES , 1963 .
[60] Joseph H. Morrison,et al. CFD Sensitivity Analysis of a Modern Civil Transport Near Buffet-Onset Conditions , 2001 .
[61] C. Ostowari,et al. Post-stall wind tunnel data for NACA 44XX series airfoil sections , 1985 .
[62] Barnes W. McCormick,et al. Aerodynamics of V/STOL flight , 1967 .