Aerospace Mechanics

Aerospace Mechanics

Journal Information


According to the latest review and ranking of the country's scientific Journals in the Islamic World Science Citation Database (ISC), the scientific Journal of Aerospace Mechanics has been ranked Q3 in terms of quality.

This Journal , which is published by the technical and engineering faculty and research institute of Imam Hossein University (AS), under license 3/2910/472 dated 5/26/ 83 of the Ministry of Science, Research and Technology under the title "Aerospace Mechanics" has been published with a scientific-research degree.

This Journal publish the latest achievements of the country's researchers, which are the result of original research and contain new results in the specialized fields of the following five main trends:

  1. Vibration dynamics and control
  2. Solid Mechanics
  3. Propulsion and heat transfer
  4. Manufacturing and Production
  5. Impact mechanics

  • Type of Access: Open Access (OA) 
  • Start of Journal : 2005
  • Credit of the Journal : Scientific-Research
  • Type of articles to be published: Research
  • Format: Print and Online
  • Frequency: Quarterly
  • Language: Persian; including English abstracts
  • Coverage: Theories, Models and Systems Related of Aerospace Mechanics
  • Type of peer-review: Double Blind Peer Review; two reviewers
  • Initial review period: 1 week
  • Average time for review articles: Maximum 20 days
  • Manual of style of the Journal : Vancouver
  • Article Processing, Publishing and judging Charges: Free for review process and Journal
  • Contact E-mail: Havafaza@ihu.ac.ir
  • Cooperation with the association: Scientific Association of High Energy Materials of Iran
  • Type of License: CC BY-NC

Audience: The audience of this Journal is made up of professors, academic faculty members of universities, experts in mechanics and related fields.

Faculty members, researchers, and graduate students are invited to prepare their Persian article according to the article preparation guide and by visiting the Journal website (http://maj.ihu.ac.ir) and registering in it, Send the electronic version of the article to the Journal office.

** Submitted articles must not have been previously published in any Journal .**

  1. Respected authors are requested to follow the format of the Journal in order to speed up the review and judging process.
  2. Respecting the rules of ethics in Journals, this Journal  is subject to the rules of the Committee on Ethics in Journals  (COPE) and follows the executive regulations of the Law on Prevention and combating fraud in Scientific Works.
  3. All articles sent to this  Journal  are reviewed by plagiarism software. Submitting the report of Samim Noor similarity  check system or Irandak similarity  check system is also necessary at the time of submitting the article. (Link to the guide to the plagiarism detector system)
  4. Also, please, when submitting the article (commitment form), (authors conflict of interest form) and form (authors' Profile) must be signed by all authors and uploaded to the system.
Current Issue: Volume 21, Issue 4 - Serial Number 82, Winter 2026 (Winter) 

Real-Time Tangent Based Path Planning for Autonomous Robots in Convex Obstacle Environments

10.47176/MAJ.2025.1520

Hesamedin Moedi, Mahdi Mozaffari, Abolfazl Manafi, Fatemeh Mahdavi G., Saeed Shamaghdari

Keywords Cloud

  • Numerical Simulation
  • Sliding Mode Control
  • genetic algorithm
  • Natural frequency
  • Buckling
  • Carbon nanotube
  • Optimization
  • Cylindrical Shell
  • Mechanical Properties
  • Inertial Navigation
  • Extended State Observer
  • Heat Transfer
  • Finite Element
  • Composite
  • Robust Control
  • Functionally graded material
  • Additive manufacturing
  • Piezoelectric
  • Kalman Filter
  • Response Surface Methodology
  • Gyroscope
  • Stability
  • Energy Absorption
  • First order shear deformation theory
  • Dynamic loading
  • Force Control
  • Triangular plate
  • Nonlinear vibrations
  • Energy harvesting
  • Chattering
  • Sliding Mode
  • differential quadrature method
  • Model Predictive Control
  • Active vibration control
  • Composite Material
  • free vibration
  • Sandwich Panel
  • Extended Kalman Filter
  • Multidisciplinary Design Optimization
  • Repeated loading
  • FGM
  • Modal Analysis
  • Sandwich panels
  • Elastic foundation
  • Flexible spacecraft
  • Guidance and Control
  • Severe plastic deformation
  • Mixing efficiency
  • Die forming
  • Structured and Un-structured uncertainties
  • Numerical Method
  • Central Composite Design
  • Grain refinement
  • CAD/CAM
  • Multi-agent system
  • Finite Element Method
  • Frequency
  • Finite Element Simulation
  • Tensegrity structure
  • Combustion Chamber
  • Spacecraft
  • Min-Max controller
  • Turbofan Engine
  • Nonlinear vibration
  • finite element analysis
  • Underactuated system with two degrees of freedom
  • neural network
  • Nonlinear Beam
  • Inertial Navigation System
  • Fuzzy Logic
  • Transverse Step
  • Trajectory Optimization
  • Free vibrations
  • Vibration
  • Numerical study
  • Integrated navigation system
  • ballistic limit
  • ANFIS
  • Shape memory alloy
  • Molecular dynamics simulations
  • Blast Loading
  • Natural Convection
  • instability
  • Backstepping Control
  • Shock tube
  • Impact
  • Experimental Investigation
  • Attitude control
  • Cylindrical shells
  • Non-Newtonian nanofluid
  • Formation control
  • Fault tolerant control
  • Experimental Test
  • Wave Propagation
  • Low velocity impact
  • Hybrid nanofluids
  • Data Fusion
  • Dynamic Analysis
  • Gas Turbine
  • Nanofluid
  • Magnetic Field
  • Rotating beam
  • Signal Processing
  • Fracture Mechanics
  • Particle Filter
  • Gaseous detonation
  • PID Controller
  • Molecular Dynamics
  • Stress Intensity Factor
  • Female die
  • Piezoelectric layer
  • Graphene
  • Nonlinear model predictive control
  • Forced Vibration
  • Interfacial shear strength
  • Fuzzy Controller
  • Underwater explosion
  • Filament collection speed
  • Force Density
  • Uncertainty
  • Image Processing
  • Terminal Sliding Mode Control
  • Predictive Control
  • Deflection
  • Turbulent Flow
  • Continuum approximation method
  • Fuzzy System
  • Jump Phenomenon
  • third order shear deformation theory
  • Multi-Objective Optimization
  • Parameter uncertainty
  • Johnson-Cook model
  • Fuzzy-PID controller
  • normal stress
  • Deep Neural Network
  • Inertial Forces
  • Vibrations Analysis
  • Hybrid Composite Laminate
  • Thrust Chamber
  • DOM
  • Corrosion
  • Generalized &alpha
  • Flight Control System
  • Adaptive backstepping approach
  • Combined actuator fault
  • Surface Mounting
  • Optimal Guidance
  • Frequency Response
  • Radial Pressure
  • Inertial Navigation System (INS)
  • 3D-Printing
  • Active steering control
  • Dynamic Performance
  • Linear Model
  • Nondestructive Test
  • mold temperature
  • Runge Kutta method
  • Adaptive sliding mode control
  • Nonlinear Programming
  • Piezoelectric Layers
  • Calorimetry
  • Extruder
  • Model uncertainty
  • Experimental study
  • Oblique blast loading
  • simultaneous symmetrical impulsive loading
  • Thick Plate
  • Film Cooling
  • Porosity
  • Channel
  • Dynamic Optimization
  • Attitude Dynamics and Control
  • critical lane change maneuver
  • Fuzzy C-Means
  • Aerodynamic Interference
  • Environmental test
  • Volumetric radiation
  • Tube based Model Predictive Control
  • Calibration
  • Cold gas thrusters
  • Emergency Condition
  • Flight Performance
  • Fuzzy approximator
  • Friction factor
  • Phase transformation models
  • Monolayer
  • Active braking control
  • Bi-Stable Composite Laminates
  • Adaptive Estimator
  • Thermodynamic simulation
  • Optimized geometry
  • Geometrical tolerances
  • Backing Material
  • Pad
  • Neural Network-Based Model Predictive Control
  • Frictional work
  • Shaped Charge
  • Robust Guidance
  • Ultra-fine-grained materials
  • Cooling flow field

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