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                             91 results found
no title author magazine year volume issue page(s) type
1 Accessibility assessment and trajectory design for multiple Near-Earth-asteroids exploration using stand-alone CubeSats Yu, Zhitong
118 C p.
 article
2 A composite system theory-based guidance law for cooperative target circumnavigation of UAVs Zhang, Min
118 C p.
 article
3 A 6-DOF sliding mode fault tolerant control solution for in-orbit autonomous rendezvous Henry, David
118 C p.
 article
4 Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight de Vries, Reynard
118 C p.
 article
5 A hybrid particle swarm optimization-gauss pseudo method for reentry trajectory optimization of hypersonic vehicle with navigation information model Wu, Yu
118 C p.
 article
6 Analysis of the post-flutter aerothermoelastic characteristics of hypersonic skin panels using a CFD-based approach Quan, Enqian
118 C p.
 article
7 Analysis on stationary window of oblique detonation wave in methane-air mixture Guo, Hongbo
118 C p.
 article
8 An efficient adjoint method for the aero-stealth shape optimization design Li, Ming
118 C p.
 article
9 An on-line deep learning framework for low-thrust trajectory optimisation Xie, Ruida
118 C p.
 article
10 An optimal steering law for sailing with solar and planetary radiation pressure Barles, Anaïs
118 C p.
 article
11 An optimization approach for improving the solar array output power of stratospheric aerostat Jiang, Yi
118 C p.
 article
12 A novel finite-time prescribed performance control scheme for spacecraft attitude tracking Gao, Shihong
118 C p.
 article
13 Approximation-free-based adaptive integral robust control with prescribed performance for unknown pure feedback system with disturbance Zhu, Bin
118 C p.
 article
14 Are nonfragile controllers always better than fragile controllers in attitude control performance of post-capture flexible spacecraft? Liu, Chuang
118 C p.
 article
15 A simultaneous use of a leading-edge fillet and a non-axisymmetrically contoured endwall in a turbine stage Turgut, Özhan H.
118 C p.
 article
16 Assessment of UAM and drone noise impact on the environment based on virtual flights Bian, Haoyu
118 C p.
 article
17 A switching-based state-scaling design for prescribed-time stabilization of nonholonomic systems with actuator dead-zones Hou, Deheng
118 C p.
 article
18 Back-propagation suppression study based on intake configuration optimization for an air-breathing pulse detonation engine Wang, Zhiwu
118 C p.
 article
19 Blow-off characteristics of a premixed methane/air flame response to acoustic disturbances in a longitudinal combustor Sun, Yongchao
118 C p.
 article
20 Buckling-driven mechanisms for twisting control in adaptive composite wings Zhang, Jiayao
118 C p.
 article
21 Catalyzed combustion of a nanofluid fuel droplet containing polydopamine-coated metastable intermixed composite n-Al/CuO Gao, Yi
118 C p.
 article
22 Combined applications of analytic methods for detection of combustion instability triggering Luong, Hung Truyen
118 C p.
 article
23 Combustion promotion and agglomeration reduction of the composite propellant using graphene Liu, Lu
118 C p.
 article
24 Control of the oscillations of shock train using boundary layer suction Petha Sethuraman, Vignesh Ram
118 C p.
 article
25 Design and analysis of a supersonic axisymmetric inlet based on controllable bleed slots Yuan, Huacheng
118 C p.
 article
26 Design and evaluation of a conical hypersonic vehicle with an overturned aerodynamic layout Xiong, Bing
118 C p.
 article
27 Design and mechanical property studies of 3D re-entrant lattice auxetic structure Shen, Jianbang
118 C p.
 article
28 Development and dynamics of a 2SPU+UPU+SP parallel rotor of helicopter Lu, Yi
118 C p.
 article
29 Dimensionality-reduction-based surrogate models for real-time design space exploration of a jet engine compressor blade Bird, Gregory D.
118 C p.
 article
30 Distributed optimal control allocation for 6-dof spacecraft with redundant thrusters Lang, Xiaoyu
118 C p.
 article
31 Editorial Board
118 C p.
 article
32 Effect of a blade end slot on supersonic compressor cascade hub-corner separation Ma, Jianci
118 C p.
 article
33 Effect of poroelastic material on vibroacoustic behavior of truncated conical shells Golzari, Masoud
118 C p.
 article
34 Effects of acoustic liner on thermoacoustic instabilities in a premixed swirl combustor Xu, Liangliang
118 C p.
 article
35 Effects of wing kinematics, corrugation, and clap-and-fling on aerodynamic efficiency of a hovering insect-inspired flapping-wing micro air vehicle Nguyen, Khanh
118 C p.
 article
36 Enhancement of wake vortex decay by air blowing from the ground Xu, Ziming
118 C p.
 article
37 Error-constrained fixed-time trajectory tracking control for a stratospheric airship with disturbances Yuan, Jiace
118 C p.
 article
38 Experimental and numerical investigation on flame propagation and transition to detonation in curved channel Pan, Zhenhua
118 C p.
 article
39 Explainable Deep Reinforcement Learning for UAV autonomous path planning He, Lei
118 C p.
 article
40 Fractional-order resolved acceleration control for free-floating space manipulator with system uncertainty Shao, Xiangyu
118 C p.
 article
41 Free vibration analysis of rotating FG-CNT reinforced composite beams in thermal environments with general boundary conditions Xu, Jiang
118 C p.
 article
42 Fuzzy-based continuous current control of electrodynamic tethers for stable and efficient orbital boost Liu, Jinyu
118 C p.
 article
43 Generalized sail trajectory approximation with applications to MagSails Bassetto, Marco
118 C p.
 article
44 Hazardous flight region prediction for a small UAV operated in an urban area using a deep neural network Jeong, Shinkyu
118 C p.
 article
45 High-precision modeling and collision simulation of small rotor UAV Zhang, Yongjie
118 C p.
 article
46 Hybrid FWPS cooperation algorithm based unmanned aerial vehicle constrained path planning Zhang, Xiangyin
118 C p.
 article
47 Ignition dynamics and combustion mode transitions in a rocket-based combined cycle combustor operating in the ramjet/scramjet mode An, Bin
118 C p.
 article
48 Improved nonlinear MPC for aircraft gas turbine engine based on semi-alternative optimization strategy Pang, Shuwei
118 C p.
 article
49 Information sparsification for visual-inertial odometry by manipulating Bayes tree Zhang, Xin
118 C p.
 article
50 Integration of path planning, trajectory generation and trajectory tracking control for aircraft mission autonomy Woo, Ji Won
118 C p.
 article
51 Intelligent sensitivity analysis framework based on machine learning for spacecraft thermal design Xiong, Yan
118 C p.
 article
52 Investigation on film cooling and aerodynamic performance of blade tip with tangential jet cooling scheme at transonic flow Zhang, Bo-lun
118 C p.
 article
53 Investigation on the drag reduction and thermal protection properties of the porous opposing jet in the supersonic flow: A parametric study with constant mass flow rate Ji, Chen
118 C p.
 article
54 Iterative two-layer thermal design strategy for step sandwich antenna of space solar power satellite using modified constrained multi-objective optimization Yang, Chen
118 C p.
 article
55 Joint estimation of target location and relative altitude from angle measurements Luo, Ji-An
118 C p.
 article
56 Landmark database selection for vision-aided inertial navigation in planetary landing missions Xu, Chao
118 C p.
 article
57 Largest recoverable component based fault recoverability of UAV swarm with removal of faulty individuals Peng, Yue
118 C p.
 article
58 Lightweight implementation of natural vibration frequency adjustment of satellite structures by varying the structural stiffness Guo, Jinsheng
118 C p.
 article
59 Mission planning for Earth observation satellite with competitive learning strategy Liu, Yuchen
118 C p.
 article
60 Noise attenuation of quadrotor using phase synchronization method Guan, Shujun
118 C p.
 article
61 Numerical and experimental flight verifications of a calibration matrix approach for load monitoring and temperature reconstruction and compensation Colombo, Luca
118 C p.
 article
62 Numerical study on the induced-ramp mixed and combustion characteristics of rocket-based combined cycle engine Jian, Dai
118 C p.
 article
63 Online midcourse guidance method for boost phase interception via adaptive convex programming Yang, Biao
118 C p.
 article
64 On the effect of the correction of modelled airfoil tonal noise for a spanwise extension du Plessis, Clarice
118 C p.
 article
65 Panel flutter mechanism of rectangular solar sails based on traveling mode analysis Liu, Zi-Xiao
118 C p.
 article
66 Performance analysis and optimal sizing of electric multirotors de Angelis, Emanuele L.
118 C p.
 article
67 Piece-wise affine MPC-based attitude control for a CubeSat during orbital manoeuvres Zhang, Xiaohua
118 C p.
 article
68 Reinforcement learning vibration control for a flexible hinged plate Qiu, Zhi-cheng
118 C p.
 article
69 Research on the influence of integrated infrared suppressor exhaust angle on exhaust plume and helicopter infrared radiation Yang, Zongyao
118 C p.
 article
70 Review of designs and flight control techniques of hybrid and convertible VTOL UAVs Ducard, Guillaume J.J.
118 C p.
 article
71 Robust adaptive sliding mode attitude control for aircraft systems based on back-stepping method Zhuang, Huixuan
118 C p.
 article
72 Robust integrated covariance intersection fusion Kalman estimators for networked systems with a unified measurement model including five uncertainties Ran, Chenjian
118 C p.
 article
73 Robust parameter estimation with outlier-contaminated correlated measurements and applications to aerodynamic coefficient identification Liu, Yuanyuan
118 C p.
 article
74 Roles of recirculating bubble on the performance of centrifugal compressors Lin, Yun
118 C p.
 article
75 Simulation of airborne collision between a drone and an aircraft nose Lu, Xiaohua
118 C p.
 article
76 Sloshing reduced-order models for aeroelastic analyses of innovative aircraft configurations Colella, Marta
118 C p.
 article
77 Spectral analysis and modelling of the spray liquid injection in a Lean Direct Injection (LDI) gas turbine combustor through Eulerian-Lagrangian Large Eddy Simulations Broatch, A.
118 C p.
 article
78 Structural damping models for passive aeroelastic control Eugeni, M.
118 C p.
 article
79 Study on unsaturated shapes of helium ballonet of rigid airship during ascent process Zhu, Qiang
118 C p.
 article
80 The flow features of Transverse Jets In Supersonic Crossflow Zhang, Ziao
118 C p.
 article
81 The spatial-temporal evolution process of flow field generated by a pulsed-DC plasma actuator in quiescent air Yang, Pengyu
118 C p.
 article
82 Three-dimensional consensus algorithm for nonsingular distributed cooperative guidance strategy Yang, Xiaoyan
118 C p.
 article
83 Transient aeroelastic response of a rotor on a sea-based oil rig during engagement operations Zhao, Jiachen
118 C p.
 article
84 Transient investigation of nozzle erosion in a long-time working hybrid rocket motor Tian, Hui
118 C p.
 article
85 Twin-fuselage configuration for improving fuel efficiency of passenger aircraft Ma, Yiyuan
118 C p.
 article
86 Unilateral alignment transfer neural network for fault diagnosis of aircraft engine Li, Bing
118 C p.
 article
87 Unsteady flows of a highly loaded turbine blade with flat endwall and contoured endwall Su, Xinrong
118 C p.
 article
88 Validation and insight of a full-scale S-76 helicopter rotor using the Lattice-Boltzmann Method van der Velden, W.C.P.
118 C p.
 article
89 Validation of transition modeling techniques for a simplified fuselage configuration Krimmelbein, Normann
118 C p.
 article
90 Vibration control of a rotating hub-plate with enhanced active constrained layer damping treatment Jiang, Fan
118 C p.
 article
91 Vortex evolution and flame propagation driven by oblique shock wave in supersonic reactive mixing layer Zhang, Dongdong
118 C p.
 article
                             91 results found
 
 Koninklijke Bibliotheek - National Library of the Netherlands