Results 11 to 20 of about 413,448 (266)

A Software-in-the-Loop Simulation of Vehicle Control Unit Algorithms for a Driverless Railway Vehicle

open access: yesApplied Sciences, 2021
The realization of the first prototype of a vehicle requires several tests of the algorithms implemented on the electronic control unit (ECU). This represents an important step for conventional vehicles, which becomes fundamental when dealing with ...
Michele Vignati   +3 more
doaj   +3 more sources

Reduced-Order Electro-Thermal Battery Model Ready for Software-in-the-Loop and Hardware-in-the-Loop BMS Evaluation for an Electric Vehicle

open access: yesWorld Electric Vehicle Journal, 2020
The software-in-the-loop and hardware-in-the-loop tests of a battery management system require a real-time compatible electro-thermal battery pack model.
An Li   +3 more
doaj   +3 more sources

Laboratory Development Approach in a 6DoF Launch Vehicle Simulation Design [PDF]

open access: yesفصلنامه علوم و فناوری فضایی, 2022
A significant challenge in developing simulation software for flying objects is managing the transition from concept design to the final stages of hardware-in-the-loop integration.
Reza Esmaelzade, Fateme Zahra Rahmani
doaj   +1 more source

Visual based GNC system from prototype to flight software [PDF]

open access: yesINCAS Bulletin, 2023
Juventas is a 6U CubeSat which is part of HERA planetary defense mission and takes advantage of an innovative visual based guidance, navigation and control (GNC) system to perform autonomous navigation in the proximity of the Didymain system.
Florin-Adrian STANCU   +4 more
doaj   +1 more source

Model-Based Approach for Automatic Generation of Hardware Architectures for Robotics

open access: yesIEEE Access, 2021
Increasingly complex robotic platforms incorporate heterogeneous sensors and actuators. They are usually coupled with embedded computers but relying on software solutions not entirely suited for processing large amount of data concurrently and fast ...
Ariel Podlubne   +4 more
doaj   +1 more source

Development and Verification of a ROS-Based Multi-DOF Flight Test System for Unmanned Aerial Vehicles

open access: yesIEEE Access, 2023
Unmanned aerial vehicles (UAVs) are used in many research fields for diverse operations, requiring the system to be safe and efficient. Therefore, the UAV system’s robustness and integrity are paramount in its design and operation.
Shinhyung Kim   +3 more
doaj   +1 more source

Guidance for Autonomous Underwater Vehicles in Confined Semistructured Environments

open access: yesSensors, 2020
In this work, we present the design, implementation, and testing of a guidance system for the UX-1 robot, a novel spherical underwater vehicle designed to explore and map flooded underground mines.
Zorana Milosevic   +3 more
doaj   +1 more source

Development Steps of Avionics and Flight Control System of Flight Vehicle

open access: yesJurnal RESTI (Rekayasa Sistem dan Teknologi Informasi), 2023
The success of a research is highly dependent on the method adopted, especially research related to dangerous and expensive matters which will certainly require special handling in the development or maintenance steps.
Herma Yudhi Irwanto   +6 more
doaj   +1 more source

Software In the Loop Simulation for Robot Manipulators

open access: yesEngineering, Technology & Applied Science Research, 2017
In the last decades, the classical verification of robotic software component is postponed until the code is developed enough to function in real hardware. For this reason, the verification of code at early stages is essential to reduce development costs and necessary time for embedded systems such as robot manipulator. Therefore, Software In the Loop (
Mossaad Ben Ayed   +2 more
openaire   +2 more sources

Linearized State-Space Model-Based Attitude Control for Rocket With Four Controllable Fins—Part 1-1: Basic Modeling and Identification

open access: yesIEEE Access, 2023
In this study, we present, analyze, and validate a linear state-space model for a simplified rocket with four fins. The model is validated experimentally using a wind tunnel. The proposed model consists of two main elements: a rocket body and fins.
Shinhyung Kim, Abera Tullu, Sunghun Jung
doaj   +1 more source

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