... is considered to validate the simulator model in low-altitude scenarios using the actual flight test results and then scale up to the stratospheric model. The geometry of the airship with different variables is presented in Table 1 . Table 1 Airship geometry parameters Variable Value...

... Turboprop engine Tractor Exhaust stub Jet flow Propeller blade Aircraft Flight test X = Length of the model(m); D = Diameter of the model(m); 3D = Three-dimensional; T_amb = Ambient temperature (deg C); Tq = Torque (%); and amb...

... and authors. The full terms of this licence may be seen at http://creativecommons.org/licences/by/4.0/legalcode Path following Flight control UAV Vector field Nonlinear guidance law Flight test In the past decade, advances in micro-electronics, sensing technology and signal processing...

... indicate side-slip angle by vibrations, whereas a sliding element inside the control stick is able to continuously indicate both angles of attack and side-slip. Design/methodology/approach Haptic feedback applied on rudder pedals and control stick were tested on a flight simulator and flight tests...

... on an aircraft ice crystal detection probe. The work included over 20 flight tests on NRC aircraft and the Airbus HAIC test programme. Jennifer Lynne Young Chalmers can be contacted at: jennifer.chalmers@nrc.ca 12 11 2018 31 12 2018 07 01 2019 © Her Majesty the Queen in Right...

... Limited 2018 Emerald Publishing Limited Licensed re-use rights only Simulation Computational fluid dynamics Crew escape system Digital human modelling Flight test Detailed methodologies specified in the report (Rucker Fort, 1975) for the computation of human mass and inertial...

... code-based approach to lay down aerodynamics could be considered as reliable to provide high angles-of-attack characteristics. Conclusions incorporate the results of a comparative analysis focusing especially on comprehensive assessment of output data quality in relation to flight tests. Originality...

... simulations and flight tests are executed for pitch angle and roll angle control of research aircraft MuPAL-α under the following fault cases: sudden reduction in aileron effectiveness, sudden reduction in elevator effectiveness and loss of longitudinal static stability. Findings The simulations...

...Jong Heon Kim; Chan Yik Park; Seung Moon Jun; Gregory Parker; Kwang Joon Yoon; Dae Keun Chung; Il Hyun Paik; Jong Rok Kim Purpose The purpose of this paper is to present the procedure and results from instrumented flight test performed on the flapping MAVs being developed by the authors. A test...