Yang Zhou

ORCID: 0000-0003-0067-5342
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About
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Research Areas
  • Spacecraft Dynamics and Control
  • Astro and Planetary Science
  • Space Satellite Systems and Control
  • Antenna Design and Analysis
  • Advanced SAR Imaging Techniques
  • Advanced Antenna and Metasurface Technologies
  • Microwave Engineering and Waveguides
  • Acoustic Wave Phenomena Research
  • Railway Engineering and Dynamics
  • Antenna Design and Optimization
  • Radar Systems and Signal Processing
  • Aerospace Engineering and Control Systems
  • Gear and Bearing Dynamics Analysis
  • Optical measurement and interference techniques
  • Solar and Space Plasma Dynamics
  • Mechanical Engineering and Vibrations Research
  • Inertial Sensor and Navigation
  • Vibration and Dynamic Analysis
  • Synthetic Aperture Radar (SAR) Applications and Techniques
  • Geophysical Methods and Applications
  • Metamaterials and Metasurfaces Applications
  • Pulsed Power Technology Applications
  • Composite Structure Analysis and Optimization
  • Topology Optimization in Engineering
  • Engineering Applied Research

National University of Defense Technology
2014-2025

Shanghai Sunshine Rehabilitation Center
2025

China Medical University
2025

Northeastern University
2018-2024

Shandong University of Technology
2024

Institute of Electronics
2020-2023

East China Jiaotong University
2021-2023

Zhejiang University
2023

University of Waterloo
2023

Singidunum University
2023

In this communication, we propose a high scanning rate leaky-wave antenna (LWA) based on slow-wave substrate integrated waveguide (SIW) structure. The effect is introduced by etching periodical slots the top surface of SIW. LWA radiation subsequently realized introducing sinusoidal modulation to profile. Such structure significantly improves due small group velocity at region. Simulation and measured results indicate that proposed scans wide angle in narrow bandwidth near cutoff frequency...

10.1109/tap.2018.2831257 article EN IEEE Transactions on Antennas and Propagation 2018-04-30

With the proliferation of unmanned aerial vehicles (UAVs) and escalating electromagnetic environment in space, there has been growing attention research focus on strong effects protection design UAVs. This paper aims to introduce potential interference that UAVs may encounter during flight. It specifically concentrates three crucial subsystems: datalink system, flight control navigation power system. The goal is provide an overview current state UAVs, along with a discussion commonly...

10.3390/electronics13020393 article EN Electronics 2024-01-17

Background Telerehabilitation is gaining popularity in European and American countries, but whether it can be successfully implemented China still lacks support from clinical studies. Objective This trial aimed to determine if a home-based telerehabilitation method clinically noninferior standard in-hospital face-to-face rehabilitation for elderly patients with total hip arthroplasty (THA) China. Methods multicenter randomized controlled was conducted January 2021 June 2022 at The First...

10.3389/fsurg.2024.1536579 article EN cc-by Frontiers in Surgery 2025-01-14

10.2514/1.g001306 article EN Journal of Guidance Control and Dynamics 2015-11-30

10.1016/j.aeue.2017.03.026 article EN AEU - International Journal of Electronics and Communications 2017-04-13

The variation principle widely used in structural dynamics analysis allows us to transform the differential equation of boundary value problem into a functional with extreme value. In recent years, it has been applied band-gap periodic structures. However, for beam-plate composite structures and ordinary boundaries, is relatively difficult traditional energy methods, such as Rayleigh–Ritz method, construct displacement functions that satisfy conditions. Hence, hybrid solution proposed this...

10.1142/s021945542150173x article EN International Journal of Structural Stability and Dynamics 2021-08-27

Fast nonsingular terminal sliding mode controllers (FNTSMCs) are proposed for underactuated spacecraft formation reconfiguration without either the radial or in-track thrust. A nonlinear dynamic model of is developed, which then linearized about circular reference orbits. Based on model, system controllability analyzed case. Due to loss control in a certain direction, disturbances consisting linearization errors and external perturbations do not enter from same channels as those inputs,...

10.1061/(asce)as.1943-5525.0000610 article EN Journal of Aerospace Engineering 2016-03-08

Electrostatically charged spacecraft accelerates when orbiting a central body with magnetic field due to the induced Lorentz force. This force could be used as propellantless propulsion for orbital maneuvers. Such is referred spacecraft. Modeling Earth’s tilted dipole rotating Earth, this paper first presents analytical expressions that characterize motion of respect inclined low Earth orbit. Using information from line-of-sight observations and gyro measurements, coupled proposed dynamical...

10.1177/0954410013511426 article EN Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering 2013-11-20

The Lorentz force acted on a charged spacecraft via interaction with planetary magnetic field provides new means of propellantless electromagnetic propulsion. Active modulation the surface charge allows to perform orbital maneuvers. By assuming Earth’s could be modeled as tilted dipole that co-rotates Earth, nonlinear dynamical model describing motion respect J 2 -perturbed orbit is developed using Lagrangian mechanics. Two potential applications proposed model, Lorentz-augmented hovering...

10.1177/0954410014537231 article EN Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering 2014-08-11

In this article, a new manoeuvring strategy for the multiple geosynchronous satellites inspection problem is proposed. contrast to previous research, it can be used visit orbiting in different orbital planes an economical way. proposed mission scenario, several chasers are initially placed equatorial high eccentric orbit. Two manoeuvres exerted at perigee adjust apogee of chaser every inspection. Subsequently, targets will visited when they fly through ascending or descending nodes their...

10.1080/0305215x.2014.979813 article EN Engineering Optimization 2014-11-14

Most of previous blind parameter estimation methods frequency hopping (FH) signals with a single channel do not adapt to overlapped signals, whereas the multi-channel-based ones are computationally much too expensive. Moreover, all single- and multiple-channel-based use batch processing techniques, they able give real-time estimates frequencies. This study establishes temporal autoregressive moving average (ARMA) model temporally FH which is then used detect hops once happen, track...

10.1049/iet-com.2010.0678 article EN IET Communications 2012-01-01
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