All Stories

  1. Modeling and Estimation of the Pitch Angle for a Levitating Cart in a UAV Magnetic Catapult Under Stationary Conditions
  2. The Application and Optimisation of a Neural Network PID Controller for Trajectory Tracking Using UAVs
  3. Identification of Differential Drive Robot Dynamic Model Parameters
  4. Explicit form of the “modified point mass trajectory model” for the use in Fire Control Systems
  5. Vehicle Navigation Systems Involving Inertial Sensors and Odometry Data from On-Board Diagnostics in Non-Gps Applications
  6. Analysis of the interaction of robots in decentralized multi-robot system for transport tasks during start of the movement
  7. Use of Standard Meteorological Messages to Simulate the Flight of 35 mm TP-T Projectile Under Actual Conditions
  8. Modeling and simulation of movement of dispersed group of mobile robots using Simscape multibody software
  9. 35 mm ammunition’s trajectory model identification based on firing tables
  10. Use of 3D Simulation to Design Theoretical and Real Pipe Inspection Mobile Robot Model
  11. Analysis of two-channel control according to the proportional navigation method
  12. The analysis of the 35 mm artillery projectile's motion model parameters' identification based on the recorded flight trajectory
  13. The effect of control signals time delays on the trajectory of a dispersed group of robots
  14. GPS-free navigation based on using inertial and odometry, data fusion and map matching algorithm
  15. The effects of the swarm configuration and the obstacles placement on control signals transmission delays in decentralized ROS-embedded group of mobile robots
  16. Calculation of aerodynamic characteristics of flying objects using Prodas and Fluent environments
  17. METEOROLOGICAL MESSAGES FOR ANTI-AIRCRAFT ARTILLERY
  18. Comparison of explicit and implicit forms of the modified point mass trajectory model
  19. Explicit “ballistic M-model”: a refinement of the implicit “modified point mass trajectory model”
  20. Effect of the mathematical model and integration step on the accuracy of the results of computation of artillery projectile flight parameters