Integral LQR Control of a Star-Shaped Octorotor

The paper starts by presenting the model of the star-shaped octorotor. LQR control is chosen to stabilize the attitude and altitude of the vehicle. Waypoint navigation is also implemented. Numerical simulations demonstra...

Tuning of the Wavelet Filters for the IMU Data Based on the PDC Method and the GPS Solution in a Bi-Dimensional Navigation Application

The degradation of navigation accuracy and integrity of GPS in the presence of radio frequency interference, hostile jamming and high dynamical situations, when the satellite signals may get lost due to signal blockage,...

Development of Framework for Acquisition of Avionics Integration Capability

With the rapid advancement in electronics technology, in the last three decades Avionics systems have evolved from standalone single function units to functionally correlated and interdependent systems. To harness the po...

An application to calculate the factors which are used to determine the tensile rupture load of a lug under axial, transverse or oblique loading

This work describes a computer application to calculate the values of the factors which are used to determine the tensile rupture load of a lug under axial, transverse or oblique loading. It can be used as a procedure fo...

An installation of technological importance at INCAS: – The air conditioning plant and its annexes