Results 41 to 50 of about 3,593,173 (338)
IEEE Access, 2023 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.
Shinhyung Kim +3 more
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Steps Towards Scalable and Modularized Flight Software for Unmanned Aircraft Systems [PDF]
, 2014 Unmanned aircraft (UA) applications impose a variety of computing tasks on the on-board computer system. From a research perspective, it is often more convenient to evaluate algorithms on bigger aircraft as they are capable of lifting heavier loads and ...
Goormann, Lukas +5 more
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Two ResNet Mini Architectures for Aircraft Wake Vortex Identification
IEEE Access, 2023 The identification of aircraft wake vortex is an essential issue in the operation of airspace utilization ratio. In particular, accurately identifying wake vortex in fine classification is helpful to guide separation standards under realistic airport ...
Siyuan Duan +3 more
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The natural history of bugs: using formal methods to analyse software related failures in space missions [PDF]
, 2005 Space missions force engineers to make complex trade-offs between many different constraints including cost, mass, power, functionality and reliability. These constraints create a continual need to innovate. Many advances rely upon software, for instance
C. W. Johnson, Johnson, C.W.
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Failure Analysis and Research of Wing Anti-ice Pressure Release on Civil Aircraft [PDF]
E3S Web of Conferences, 2021 CAS alert message ‘PSW FAIL’ shows up frequently during civil aircraft test flights. This thesis provides an in-depth study of the problem by describing the fault phenomena and analyzing the fault based on historical data, system principles, and fault ...
Wang Jian
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, 2021 Developing flight software has often presented many challenges. Previously, flight software was designed from scratch for each mission which was expensive and time-consuming.
Ray Umawing, Joseph +1 more
core
SINBAD flight software, the on-board software of NOMAD in ExoMars 2016 [PDF]
SPIE Proceedings, 2016 The Spacecraft INterface and control Board for NomAD (SINBAD) is an electronic interface designed by the Instituto de Astroffisica de Andalucfia (IAA-CSIC). It is part of the Nadir and Occultation for MArs Discovery instrument (NOMAD) on board in the ESAs ExoMars Trace Gas Orbiter mission. This mission was launched in March 2016.
Pastor-Morales, M. C. +22 more
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Космические аппараты и технологии, 2020 At present, the daily and combat activities of almost any army in the world are largely determined by the quality of information and space support. At the same time, the quality of support depends largely on the stability of the functioning of such ...
M. A. Prokhorov +2 more
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An Efficient Design-to-Verification Framework for CubeSat ADCS: Application to INHA RoSAT
AerospaceCubeSats are increasingly adopted for space missions due to their low cost and short development cycles. However, their attitude determination and control systems (ADCS) often suffer from limited verification environments and constrained hardware ...
Hye-Eun Yoo +4 more
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International Journal of Aviation, Aeronautics, and Aerospace, 2018 All pilots are required to calculate aircraft performance parameters prior to flight. This includes takeoff and landing distances. Traditionally, pilots in training have planned for takeoff and landing performance using paper charts provided by the ...
Tyler A Babb, Christina Hiers
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