Sharif Digital Repository

The analysis results of air combat simulations explain fighters succeed at close air combat that are super maneuverable and at high angle of attack controllable. Closed-coupled delta wing/canard configurations play an important role in modern aircraft design. These configurations offer high trimmed lift, improved agility and maneuverability as well, as a potential for increased lift-to drag ratio, all of which make them attractive to study. Experiments were carried out in a subsonic closed circuit wind tunnel over a delta wing model under the influence of canard. Canard was set in two different vertical positions, high and mid, with respect to the wing location. Flowfield measurements were... 

This work investigates the possibility of developing suitable design guidelines for aircraft flying in very low altitude as well as terrain following flights (TFF). The work aims to highlight the TFF mission in the early stages of design process; as oppose to other mission conducted by the aircraft. Current approach in TFF relies heavily on efficient Flight Control System (FCS) regardless of the overall configuration of aircraft. However, in this work, we show not all aircraft in the service could conduct TFF and maneuverability of airplane is very important. In fact, we investigate the overall impact of TFF on the wing loading (W/S) and thrust loading (T/W); if we were to design an aircraft... 

Ship maneuvering simulation and prediction in preliminary design stages has been concerned since forty years ago due to accidents occurred to large vessels and so many efforts have been held to develop the methods for simulation of ship maneuvering. Standards concerning ship maneuvering have been presented by International Maritime Organization that is known as a criteria to evaluate maneuvering performance of the ships. Traditionally ship maneuvering has been simulated in deep water and without any environmental conditions such as wind, wave, marine currents and effects resulted by asymmetric flow around ship hull during waterway entrance and shallow waters. Furthermore by introducing the... 

Up to now many different mechanisms have been proposed for a swimming micro robot, but most of the previously designed micro robots are not able to perform three- dimensional maneuver and the motion of the proposed swimmers are limited along a straight line or in a plane. Some important issues that must be ruled in designing micro robots include: reduced number of actuators, high maneuverability, high motion controllability and elimination of lateral drift. In this study the aim is to design a micro swimmer with the aforementioned capabilities as much as possible. In this regard, many different ideas based on the quadrotor motion, flagellated bacteria and spiral flagellated bacteria, Fish... 

Helical swimming robots with a capable propulsion system at low Reynolds numbers have been proposed for many applications. Although linear propulsion characteristics of swimming robots with a single helical flagellum have been extensively studied, the characteristics of maneuverability have not been completely investigated yet. In this thesis two novel mechanisms was proposed. The first mechanism presents a new method for the maneuverability of the helical swimming robot with a single helical flagellum. This mechanism is based on the change in the angle between the helical and body axes. This study shows that a change in the aforementioned angle can enable the swimming robot to have turning... 

This project deals with the design, fabrication and control of a tilting-rotor quadrotor. This type of UAV can have high maneuverability in all 6 degrees of freedom (3D attitude and 3D position). The rotor axes can be tilted independently to produce desired force and torque vectors. This capability resolves limitations of the classic quadrotors and provides independent control of orientation and position. To control this UAV, we have proposed a control scheme relating the desired trajectory to the required forces and torques. Then a PID controller for the simultaneous control of position and attitude is designed. This controller is tested in a simulation and the results show that the control...