Sentence examples for attitude control hardware from inspiring English sources
The capabilities of microsatellite attitude control hardware have considerably evolved during the last two decades.
Increasing the satellite agility, without changing the attitude control hardware, can be accomplished by using optimal control to design shortest-time maneuvers.
In order to mitigate the risks associated with design and verification of the highly demanding agile attitude control, experimental results involving a hardware in-the-loop demonstrator are presented.
This paper accomplishes one goal and it was to verify and to validate a Spin Magnetic Attitude Control System (SMACS) program and to perform Hardware-In-the-Loop (HIL) air-bearing experiments.
The paper describes in detail the design and implementation of the attitude control system of a small satellite, focusing on the hardware and software aspects.
The magnetic spin rate control approach is able to perform spin rate control and it is verified with an Attitude Control System (ACS) air-bearing MATLAB® SIMULINK® model and a hardware-embedded LABVIEW® algorithm that controls the spin rate of the test platform on a spherical air bearing table.
The flight system consists of hardware and software elements including RF communications, power system, attitude control, command and data handling, thermal control and mechanical structures.
Simulation and Hardware-in-Loop experiments proved the feasibility of the proposed attitude control system.
Since they have less control hardware, they are cheaper to maintain and are generally more accurate.
We propose a modular framework that combines orbital mechanics, attitude control and scheduling optimization to plan the time-varying, full-body orientation of agile Cubesats in a constellation such that they maximize the number of observed images and observation time, within the constraints of Cubesat hardware specifications.
