HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS
Sign Up to like & getrecommendations! Published in 2018 at "CEAS Aeronautical Journal"
DOI: 10.1007/s13272-018-0294-3
Abstract: HALO (High Altitude and Long Range Research Aircraft), the atmospheric research aircraft of the German Aerospace Center (DLR), can be equipped with under-wing stores at different wing positions to transport scientific instruments for atmospheric research.… read more here.
Keywords: aircraft; wing stores; system; flight ... See more keywords
Flight Test Results of Disturbance Attenuation using Preview Feedforward Compensation
Sign Up to like & getrecommendations! Published in 2017 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2017.08.2086
Abstract: Abstract This paper demonstrates flight test results of disturbance attenuation of an aircraft by preview control, which was explained and its hardware-in-the-loop (HIL) simulation results were reported in a previous paper. The design methodology of… read more here.
Keywords: test results; results disturbance; flight test; preview ... See more keywords
Flight test assessment of L1 and dual-frequency multi-constellation SBAS for civil aviation in Australia
Sign Up to like & getrecommendations! Published in 2025 at "Journal of Navigation"
DOI: 10.1017/s0373463324000389
Abstract: Abstract This paper analyses the performance of the Australian and New Zealand Satellite-Based Augmentation System (Aus-NZ SBAS) test-bed to evaluate its use in civil aviation applications with a focus on dual-frequency multi-constellation (DFMC) signals. The… read more here.
Keywords: flight test; flight; test; civil aviation ... See more keywords
Development and Verification of a ROS-Based Multi-DOF Flight Test System for Unmanned Aerial Vehicles
Sign Up to like & getrecommendations! Published in 2023 at "IEEE Access"
DOI: 10.1109/access.2023.3267128
Abstract: Unmanned aerial vehicles (UAVs) are used in many research fields for diverse operations, requiring the system to be safe and efficient. Therefore, the UAV system’s robustness and integrity are paramount in its design and operation.… read more here.
Keywords: system; development; flight test; flight ... See more keywords
Low-Earth Orbit Flight Test of an Inflatable Decelerator Overview and Science Return
Sign Up to like & getrecommendations! Published in 2025 at "Journal of Spacecraft and Rockets"
DOI: 10.2514/1.a36147
Abstract: The Low-Earth Orbit (LEO) Flight Test of an Inflatable Decelerator (LOFTID) mission was the culmination of two decades of research and development for Hypersonic Inflatable Aerodynamic Decelerator (HIAD) technology. With its unique 6m diameter inflatable… read more here.
Keywords: flight test; decelerator; earth orbit; flight ... See more keywords
Flight Test Techniques for Quantifying Pitch Rate and Angle of Attack Rate Dependencies.
Sign Up to like & getrecommendations! Published in 2017 at "Journal of aircraft"
DOI: 10.2514/1.c034407
Abstract: Three different types of maneuvers were designed to separately quantify pitch rate and angle of attack rate contributions to the nondimensional aerodynamic pitching moment coefficient. These maneuvers combined pilot inputs and automatic multisine excitations, and… read more here.
Keywords: pitch rate; rate angle; flight; flight test ... See more keywords
Determining Aircraft Moments of Inertia from Flight Test Data
Sign Up to like & getrecommendations! Published in 2021 at "Journal of Guidance, Control, and Dynamics"
DOI: 10.2514/1.g006072
Abstract: Flight test maneuvers and dynamic modeling techniques were developed for determining aircraft moments of inertia from flight test data. Full nonlinear rigid-body rotational equations of motion were... read more here.
Keywords: aircraft moments; flight; flight test; moments inertia ... See more keywords
Validation of a Small UAV Dynamic Model Using CFD and Flight Test Data
Sign Up to like & getrecommendations! Published in 2025 at "Periodica Polytechnica Transportation Engineering"
DOI: 10.3311/pptr.41190
Abstract: Fixed-wing Unmanned Aerial Vehicles (UAV) are increasingly utilized in various missions requiring stable and responsive performance. Accurate dynamic models are essential to ensure effective UAV control. This study presents the development and validation of a… read more here.
Keywords: flight test; test data; flight; uav dynamic ... See more keywords
Predicting Workload Experienced in a Flight Test by Measuring Workload in a Flight Simulator.
Sign Up to like & getrecommendations! Published in 2019 at "Aerospace medicine and human performance"
DOI: 10.3357/amhp.5350.2019
Abstract: BACKGROUND: In order to determine the minimum flight crew number and show compliance with airworthiness regulations, the workload of flight crew should be measured in various flight scenarios both in a simulator and in flight… read more here.
Keywords: workload experienced; flight; workload; flight test ... See more keywords