Results 31 to 40 of about 1,035,424 (313)
Biologically Inspired Feedback Design for Drosophila Flight [PDF]
, 2007 We use a biologically motivated model of the Drosophila's flight mechanics and sensor processing to design a feedback control scheme to regulate forward flight.
Dickinson, Michael H. +6 more
core +1 more source
Xibei Gongye Daxue Xuebao, 2021 To overcome the lack of robustness of the nonlinear dynamic inversion (NDI) control, a simple and practical adaptive NDI control method based on an improved piecewise constant is proposed in this paper to enhance its robustness to disturbances and ...
doaj +1 more source
Overview of Electric Propulsion Motor Research for EVTOL
Engineering ProceedingsElectric aviation is the future development direction of aviation industry technology. Electric vertical take-off and landing aircraft(eVTOL) is an important carrier of electric aviation, whose technology research and development, processing and ...
Xiaopeng Zhao +4 more
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Output Feedback Fuzzy Gain Scheduling for MIMO Systems Applied to Flexible Aircraft Control
AerospacePrevious works by our group evidenced stability problems associated with flight control law design for flexible aircraft regarding gain scheduling.
Guilherme C. Barbosa +1 more
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A Low-Cost Voltage Surge Monitor with Temperature Compensation for Electrified Aircrafts
Engineering ProceedingsAlong with the trend of aircraft electrification, the penetration of power electronics converters in aircraft energy systems is gradually deepening.
Zhao Song +3 more
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On inertial navigation and attitude initialization in polar areas
Satellite Navigation, 2020 Inertial navigation and attitude initialization in polar areas become a hot topic in recent years in the navigation community, as the widely-used navigation mechanization of the local level frame encounters the inherent singularity when the latitude ...
Yuanxin Wu, Chao He, Gang Liu
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Practical aspects of modeling aircraft dynamics from flight data [PDF]
, 1984 The purpose of parameter estimation, a subset of system identification, is to estimate the coefficients (such as stability and control derivatives) of the aircraft differential equations of motion from sampled measured dynamic responses. In the past, the
Iliff, K. W., Maine, R. E.
core +1 more source
FEBS Letters, EarlyView.Structural and biochemical characterisations show that the planar cell polarity (PCP) protein Inturned harbours a unique PDZ‐like domain that does not bind canonical PDZ‐binding motifs (PBMs) like that of another PCP protein Vangl2. In contrast, the apical‐basal polarity protein Scribble contains four PDZ domains that bind Vangl2, but one PDZ domain ...
Stephan Wilmes +4 more
wiley +1 more source
Energy-oriented architecture optimization method for aircraft
Hangkong gongcheng jinzhanMulti-electric/all-electric flight vehicles usually face problems such as the complexity of coupling between systems, the overall energy efficiency and the economic balance. An energy-optimal architecture optimization method for aircraft is proposed.
SONG Yichuan +4 more
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Research on Aircraft Surface Taxi Path Planning and Conflict Detection and Resolution
Journal of Advanced Transportation, 2021 Aircraft surface taxiing conflict avoidance is mostly adopted by waiting and rerouting methods, but this method does not consider the difference in total taxiing time that may be caused by different strategies.
Ningning Zhao, Nan Li, Yu Sun, Lei Zhang
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