Purpose Attitude determination and control subsystem (ADCS) is a vital part of earth
observation satellites (EO-Satellites) that governs the satellite's rotational motion and …

Conformal antenna arrays have long represented an attractive solution to challenges
imposed by an electromagnetic aperture on an aerospace platform. This allows designers to …

In the space missions according to uncertainties in the satellite dynamics, and due to effects
of the uncertainties on satellites attitude control, an adaptive control is effective and useful …

In this paper focused on design of a second order sliding mode controller for a fixed wing
airplane using real twisting algorithm. Simple sliding mode controller creates chattering in …

Future space missions will rely on novel high-performance computing to support advanced
intelligent on-board algorithms with substantial workloads that mandates firm real-time and …

Fuel slosh dynamics can disturb attitude of spacecraft which has a partially filled container,
in orbital maneuvering. So, it is necessary to control this harmful phenomenon. This paper …

Remote sensing satellites propulsion subsystem preliminary design based on performance
sizing is discussed. The process is a fairly complicated one considering a variety of …

This thesis is the product of an effort to develop a CubeSat Conceptual Design Tool for the
California Polytechnic State University CubeSat Laboratory. Such a tool is necessary due to …

Background and Objectives: At the present time, the industry of space systems design,
manufacture and launch has fallen out of favor with governments and numerous private …

پیشینه و اهداف: در زمان حاضر صنعت طراحی و ساخت و پرتاب ماهواره از انحصار دولت‌ها خارج شده و
نمایندگان متعدد بخش خصوصی در سراسر دنیا در حال رقابت با یکدیگر برای تصاحب سهم …‎