This paper presents the system identification by physical’s law method and designs the controller for the Azimuth Angle Control of the Platform of the Multi-Launcher Rocket System (MLRS) by Root Locus technique. The plant mathematical model was approximated using MATLAB for simulation and analyze the system. The controller proposes the implementation of PID Controller using Programmable Logic C...

The problem of finite element modeling and analysis of dynamic interactions between the launcher and a remotely piloted aircraft structure is considered. The governing equations of motion are shown to constitute a set of ordinary differential equations with time varying structural matrices. An iterative strategy that treats separately the dynamics of the launcher and the aircraft is developed. ...

The navigation is a critical element of a satellite launcher. The objective of this research is to evaluate the additional precision and robustness provided to the navigation solution by using the reference trajectory data. To include this information, the error state model of a GPS/INS configuration is augmented to estimate the difference between the launcher and the reference trajectory attit...

The manipulation of surface plasmon polariton (SPP) propagation is a basic subject for the realization of novel optical devices. Although the unidirectional SPP launcher has been demonstrated, it has been difficult to realize active control suitable for device applications. Here, we propose a graphene device with electrically controllable propagation of SPPs. The source/drain electrode of this ...

The next generation of space systems will have to achieve more and complex missions. In order master the development cost duration such systems, an alternative a manual design is automatically synthesize main parameters system. this paper, we present approach for specific case scheduling flight control launcher. requires two successive steps: (1) formalization problem be solved in parametric fo...

Abstract In order to evaluate the anti shock overload ability of electronic components and parts in explosive device launcher, half sine wave generator with certain amplitude pulse width is often used verify it. this paper, gun launcher as generator. Different charge structures are studied for interior ballistics process barrel or without venting according requirements mechanical overload. The ...