Milan Vrdoljak

Aerodynamic model of a modern fighter aircraft for subsonic speeds

Performance comparison for two passenger airplanes

Static stability and trim flight analysis for unmanned aircraft with lifting wing configuration

Analysis of aerobatic airplane performance with total energy method

Aircraft flight simulation in system failure emergency with air traffic management interaction

Vortex lattice method for a lifting surface with deflected control surfaces

Parallel flight simulation of a fighter aircraft and an anti-aircraft missile in a selected scenario

Performance of large amphibious firefighting airplane

Analysis of adaptive and robust control of a modern fighter aircraft

Unguided rocket upgrade with control elements

Analysis of crewed spaceplane landing after re-entry from orbit

Analysis of realistic atmospheric conditions varying with altitude on artillery projectiles flight

Supersonic aerodynamics model for modern fighter aircraft

Vortex lattice method for a lifting surface with complex geometry

Implementation of fly-by-wire flight controls on flight simulator for modern fighter airplane

Longitudinal linear flight model for firefighting airplane

Analysis of trimmed atmospheric flight for crewed spacecraft in descent and landing approach phase

Analysis of uncertainty influence of aerodynamic coefficients estimation on artillery projectile impact points

Helicopter flight model based on point mass model

Analiza senzitivnosti parametara generičkog modela leta helikoptera

High-angle-of-attack aerodynamics model for modern fighter aircraft

Unaprjeđenje uzdužnog aerodinamičkog modela aviona opće avijacije s modelom povijanja struje i utjecaja tla

Extended unsteady aerodynamic interference model of formation flight

Sailplane performance analysis

Suitability analysis of additive technology application for production of airfoil wind tunnel test model

Comparison of the destructive power of 5.56x45 and 7.62x39 bullets

Estimation of drag and selected performance of four-passenger seaplane

Pilot workload analysis for modern fighter aircraft from the flight simulator experiment

Analysis of trimmed flight and static stability of four-passenger seaplane

Elements of autonomous flight control and guidance of the modern fighter aircraft

Control system design for autonomus unmanned aerial vehicle and its review with flight simulation application

Performance analysis for sailplane with optional electric propulsion

Simulations comparison of constant stohastic wind effects on an unguided rocket using different probability distributions

Aircraft flight simulation with point mass model

Influence analysis of different distributions of manufacturing error as a stohastic parameter on flght of unguided rocket

Aerodynamic characteristics of canard-wing configuration

The effect of mass unbalance and thrust force asymmetry on the dispersion of unguided projectile hits

Subsonic flight simulation for modern fighter aircraft

Effect of Disturbances in Atmospheric Condition on the Projectile's Trajectory Deviation

The Effect of Manufacturing Errors on the Projectile Stability

Aircraft trim and performance analysis based on aerodynamic model identified from flight test

Influence of runway realistic conditions on take-off distance

Aerodynamic characteristics of tandem wing configuration

Workload and handling quality ratings for fighter aircraft

Subsonic trimmed flight characteristics of modern fighter aircraft with canard-wing configuration

Aircraft trim assessment from flight simulator experiment

Performance of unmanned combat aerial vehicle

Development of flight model for a general aviation airplane and its aplication for flight simulator

Stability analysis of long-range VTOL unmanned areal vehicle

Static stability and trim analysis for electric propeller business aircraft

Flight simulation of general aviation aircraft in non-standard atmosphere with wind

Dispersion analysis for the long-range rifle bullet

Flight model for the anti-aircraft missile

Ground effect on unmanned aircraft performance and trim

Performance analysis for electric propeller business aircraft

Icing effects on aircraft performance and trim

Estimation of the fighter aircraft range

Performance of the ultralight aircraft with hybrid-electric propulsion system

The Analysis of Impact of the Infantry Bullets of Different Calibers on Poorly Sheltered Targets

Analysis of Aircraft Performance in Climb With Application of Total Energy Method

Performance analysis for modern fighter aircraft

Analysis of Anti-tank Rocket Flight With Six Degrees of Freedom Model

Flight simulation of a sailplane with the pilot in the loop

Helicopter trim analysis

Aircraft performance in non-standard atmosphere and in atmosphere with wind

Flight simulation of a radio-controlled aircraft

Motion of center of mass of an airplane in cruise at large distances

Application of Six Degrees of Freedom Flight Model for Dispersion Analysis of Artillery Projectile

Dispersion Analysis of Artillery Projectiles Hits with Application of MPMM model

Aircraft mission analysis from aspect of fuel economy

Comparison of Modified Point Mass Model and Euler Flight Model

Performance of conventional helicopter configuration with wings

Performance analysis of electric aircraft

Quasi-steady Rotor Dynamics Model and Application to Helicopter Flight Model

Aerodynamic Interference Analysis for the Aircraft in Formation Flight With Application of Vortex Lattice Method

Flight Simulation of Tank Projectile

Analiza protoka helikopterskog rotora primjenom modela Mangler-Squire

Application of Blade Element Theory for Aircraft Propellers

Propeller aerodynamic characterstics analysis with application of blade element momentum theory

Static stability and trim analysis for ultra-light aircraft

Comparison of different tail configurations with application of the lifting line method

Direction Control System for Unmanned Aircraft with Flying Wing Configuration

Vortex lattice method for the lifting surface with simple geometry

Performance analysis for the unmanned aerial vehicle HUSZ Tern

Lift analysis for the body-lifting surface arrangement

Aerodynamic Interference Analysis of Mixed Close Formation Flight

Selected Performance Analysis for the Helicopter With Coaxial Rotor

Analiza polijetanja male radio-upravljane letjelice

Croatian Aviation Terminology

Analysis of Longitudinal Static and Dynamic Stability for Commuter Floatplane

On the influence of the changing state of the atmosphere above the fire site on performance of the helicopter

Closed-form model of helicopter rotor

Metoda za praćenje aerodinamičkih značajki transportnog zrakoplova tijekom eksploatacije

Helicopter Performance in Autorotation

Analiza utjecaja tla na aerodinamičke značajke krila primjenom metode noseće linije

Performance of Unmanned Autogyro

Design of Helicopter for Emergency Medical Service

Visualization of Helicopter Rotor Motion with Interactive Control

Flight Model for Unmanned Aircraft with Flying Wing Configuration

Conceptual design of transport helicopter

Analysis of the helicopter rotor in vertical flight with application of lifting line theory

Stability analysis of small aircraft with flying wing configuration

Analysis of aerodynamic coefficients for supercritical airfoil

Application of the lifting line theory on the complex wing geometry

6DOF Model of Quadrotor Helicopter

About the risks of helicopter utilization in firefighting activities from the flight mechanics point of view

Flight planning of the fighter aircraft with the application of the steady state flight model

Analysis of aerodynamic load loads on the tail for the NOTAR helicopter configuration

Visualization of helicopter rotor motion and control as an additional e-learning curriculum material

Dynamic stability analysis of the radio-controled aircraft

Helicopter Flight Model

Helicopter Flight Real-Time Simulation with level one model

Primjena teorije elementarnog kraka za analizu rotora helikoptera u vertikalnom i horizontalnom letu

Performance analysis of the transport turbo-prop aircraft

Dynamic Simulation of Landing Elastic Airplane

Flying and handling qualities analysis for transport aircraft

Calculation of the transport airplane performanses

Stress analysis of a watertower