Source record · English / Chinese original · 14
Original website text is reproduced below in its source language. Translated introductions are reading guides, not a full translation of the source. Confirm the configuration and operating conditions for your project.
System Overview
本平台為一套 硬體在環 (Hardware-in-the-loop, HIL) 測試系統，整合實體動力組件與虛擬飛行模擬軟體。透過實測馬達與螺旋槳產生的真實推力並即時回饋至模擬器，實踐虛實整合驗證，以降低研發成本與墜機風險。
This platform is a Hardware-in-the-Loop (HIL) testing system that integrates physical powertrain components with virtual flight simulation software. By measuring the real thrust generated by the motor and propeller and feeding it back into the simulator in real time, it achieves virtual-real integrated verification to reduce R&D costs and crash risks.
Target UAV
機型類別：長航程偵察與高機動無人機 (FPV)。
重量等級：最大起飛重量 (MTOW) 2kg 至 5kg。
性能要求：支援極速 140km/h 以上之動態響應測試。
環境模擬：需能模擬至少 七級風 的干擾條件。
Aircraft Category: Long-endurance reconnaissance and high-maneuverability FPV drones.
Weight Class: Maximum Take-Off Weight (MTOW) 2 kg to 5 kg.
Performance Requirements: Supports dynamic response testing at top speeds over 140 km/h.
Environmental Simulation: Capable of simulating disturbance conditions up to at least Beaufort Force 7 winds.
Structure
The published platform measures propulsion behavior through dedicated test hardware. Use it to discuss the motor, propeller, power source and measurement conditions as a matched system, with agreed test outputs.
Explore this systemUNI-CO TECH / Discuss your requirements
Describe the site, task, payload and operating constraints. Your request is saved in the platform inbox for review and assignment.
Your contact details and attachments are accessible to authorized platform administrators for handling this request. No supplier notification is sent automatically. For access or deletion requests, use the platform privacy contact.
Privacy & request handling