C. A. Osheku

Validating a Novel Theoretical Expression for Burn time and Average Thrust in Solid Rocket Motor Design

B. K. Aliyu, C. A. Osheku, E. O. Oyedeji, M. A. L. Adetoro, A. A. Okon & C. M. Idoko · Advances in Research · 2015

A major application of solid propellants is in gun propulsion systems and rockets. The performance of a rocket depends greatly on the design of the solid propellant that meets a specific mission. Performance characteristics such as the burn time, burn rate, average thrust, specif...

Open access Research Article 10.9734/AIR/2015/18468

Oscillation Analysis for Longitudinal Dynamics of a Fixed-Wing UAV Using PID Control Design

B. K. Aliyu, C. A. Osheku, P. N. Okeke, F. E. Opara & B. I. Okere · Advances in Research · 2015

A longitudinally disturbed motion of a UAV after an arbitrary initial disturbance consists normally of two oscillatory modes: the short-period oscillation and the phugoid oscillation.The typical longitudinal model of a UAV in state-space can be separated into short-period mode an...

Open access Research Article 10.9734/AIR/2015/18334

Identifying Stiff Ordinary Differential Equations and Problem Solving Environments (PSEs)

B. K. Aliyu, C. A. Osheku, A. A. Funmilayo & J. I. Musa · Journal of Scientific Research and Reports · 2014

Stiff Ordinary Differential Equations (SODEs) are present in engineering, mathematics, and sciences. Identifying them for effective simulation (or prediction) and perhaps hardware implementation in aerospace control systems is imperative. This paper considers only linear Initial...

Open access Research Article 10.9734/JSRR/2014/9842