Zhaojun Pang

ORCID: 0000-0002-8520-7814
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About
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Research Areas
  • Space Satellite Systems and Control
  • Astro and Planetary Science
  • Planetary Science and Exploration
  • High-Velocity Impact and Material Behavior
  • Control and Dynamics of Mobile Robots
  • Energetic Materials and Combustion
  • Spacecraft Dynamics and Control
  • Electromagnetic Launch and Propulsion Technology
  • Mechanical Engineering and Vibrations Research
  • Structural Response to Dynamic Loads
  • Nonlocal and gradient elasticity in micro/nano structures
  • Mechanical Behavior of Composites
  • Numerical methods in engineering
  • Ion-surface interactions and analysis
  • Natural Fiber Reinforced Composites
  • Mechanics and Biomechanics Studies
  • Guidance and Control Systems
  • Fluid Dynamics Simulations and Interactions
  • Cellular and Composite Structures
  • Aerospace Engineering and Control Systems
  • Chaos control and synchronization
  • Mechanical stress and fatigue analysis
  • FinTech, Crowdfunding, Digital Finance
  • Recommender Systems and Techniques
  • Robotic Mechanisms and Dynamics

Nanjing University of Science and Technology
2016-2025

Hangzhou Normal University
2025

Indiana University School of Medicine
2025

Songjiang District Central Hospital
2025

Shanghai Jiao Tong University
2025

China National Petroleum Corporation (China)
2024

Xi'an University of Science and Technology
2024

Nanjing University of Aeronautics and Astronautics
2015-2016

To address the negative impact of excessive forces during penetration space debris by harpoon attachment devices, causing damage to rear electronic components, research has been conducted on buffering and energy absorption effects 2A12 aluminum honeycomb. A simulation model for honeycomb crushing was established through alloy quasi-static tests, SHPB dynamic compression tests. The study investigated effect response accelerations in device results show that at launch velocities 29.2 m/s 29.6...

10.1177/10996362251315086 article EN other-oa Journal of Sandwich Structures & Materials 2025-01-14

This paper presents an advanced multiple pieces of debris capture method for the tethered space net robot. A novel strategy that integrates redeployment and self-assembly techniques is introduced. With this strategy, robot self-assembles to close pocket quickly maneuvers nearby target debris. Upon reaching its target, redeploys capture. Central approach development a capturing model accurately describes state function deployed incorporates effective dragging counteract bouncing. To enable...

10.2514/1.g007908 article EN Journal of Guidance Control and Dynamics 2024-05-14

In this paper, a new mission model, called multi-debris active removal with partial debris capture strategy, is proposed. The model assumes that platform only captures part of the scheduled at time and then releases these pieces to disposal orbit. This process repeated until all removed. A genetic algorithm multi-parameter concatenated coding method designed optimize plan strategy. set six 10 are selected demonstrate proposed planning method. result confirms effectiveness provides more...

10.1016/j.cja.2023.03.013 article EN cc-by-nc-nd Chinese Journal of Aeronautics 2023-03-10

Abstract In this study, we introduce a kind of Stancu variant the complex Bernstein-Durrmeyer-type operators in movable compact disks. Their approximation properties for analytic functions disks are investigated.

10.1515/dema-2024-0092 article EN cc-by Demonstratio Mathematica 2025-01-01

Aiming at the problem of harpoon attachment harpoons to space debris with aluminum honeycomb as skin in space, this paper studies penetration-harpoon effect three kinds on sandwich plate under low-velocity impact environment by means experiment and numerical simulation. Penetration tests plates were carried out ground wingless, double-winged three-winged harpoons. The results show that more wings harpoon, larger reaming generated during penetration process, stronger ability. A finite element...

10.1177/10996362251341075 article EN Journal of Sandwich Structures & Materials 2025-05-05

Developing conductive hydrogels has led to significant advancements in bioelectronics, especially the realms of neural interfacing and neuromodulation. Despite this progress, synthesis that simultaneously exhibit superior mechanical stretchability, robust bioadhesion, high conductivity remains a challenge. Traditional approaches often resort filler concentrations achieve adequate electrical conductivity, which detrimentally affects hydrogel's integrity biocompatibility. In study, we present...

10.1021/acsnano.5c03336 article EN ACS Nano 2025-05-07

Tether-net is a promising active debris removal technique, and closing mechanism can ensure the reliable wrapping of space by using tether-net. This study focuses on dynamics model split sliding joint between thread ring. First, new kind proposed, which drives to close net mouth through masses, mass-spring-damper method used Thereafter, for first time, thread-ring proposed based method, be simulate process Finally, one-edge closure experiment carried out experimental results are compared...

10.1155/2021/8827141 article EN cc-by International Journal of Aerospace Engineering 2021-01-02

The space harpoon is a rigid-flexible, coupled debris capture method with simple, reliable structure and high adaptability to the target. For process of impacting embedding into target plate, effect friction at low-velocity impact studied, criteria for effective corresponding launch velocity are determined. A simulation model dynamics plate considering tangential established, reliability numerical verified by comparing test, focusing on kinetic energy change length during harpoon. results...

10.3390/ma15145041 article EN Materials 2022-07-20

This paper studies the chaotic motions of a tethered satellite system by utilizing ground-based experimental system. Based on dynamics similarity principle, dynamical equivalent model between on-orbit and its ground physical is obtained. As result, space environment can be simulated via thrust forces torque momentum wheel simulator. The numerical results show attitude motion mother satellite. experiment shows that as negative damping able to suppress motion.

10.1088/1742-6596/744/1/012116 article EN Journal of Physics Conference Series 2016-09-01

Purpose This paper aims to study the encounter issues of Tethered-Space Net Robot System (TSNRS) with non-target objects on orbit during maneuver, including collision small space debris and obstacle avoidance from large obstacles. Design/methodology/approach For TSNRS debris, available model tethered net its limitation is discussed, detection method improved. Then dynamic response studied a closed-loop controller designed. avoidance, variable enveloping circle has coupled artificial...

10.1108/aeat-07-2021-0208 article EN Aircraft Engineering and Aerospace Technology 2022-01-08

The paper deals with the deployment dynamics of a tethered spacecraft consideration attitude motion. flexible tether is modeled through sequence lumped masses connected by viscoelastic dampers, and as rigid body. According to Newtons law, time-varying equations motion system for retrieval are obtained. Then, during numerically investigated based on Kissels strategy. results show that greatly dependent initial angle spacecraft. If without control action tethers deployment, impulse arisen form...

10.1360/132012-901 article EN Zhongguo kexue. Wulixue Lixue Tianwenxue 2014-07-01

Power-form nonlinear contact force models are widely adopted in relatively moving parts of macro (e.g., rolling bearings considering Hertzian restoring between elements and bearing raceways) or micro the cantilever probe system atomic microscopy) scale mechanical systems, resonance could cause serious problems wear, fatigue, vibration, noise, which has attracted widespread attention. In present paper, softening/hardening stiffness characteristics continuous one-sided power-form spring...

10.3390/app11167722 article EN cc-by Applied Sciences 2021-08-22

A novel nonlinear model of single-layered graphene sheets (SLGSs) subject to large deformation is proposed using the absolute nodal coordinate formulation (ANCF) and nonlocal elasticity theory. The geometrical definition SLGSs described by ANCF thin plate element while strain energy expressed Then, elastic force Jacobian derived. We verify comparing results with other published conduct corresponding numerical case study clarify influence boundary conditions (BCs), parameters, side length...

10.1142/s1758825119500376 article EN International Journal of Applied Mechanics 2019-04-22
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