Software-in-the-loop investigation of wake-vortex-encounter-response of identical multirotor pair with PX4 attitude controller

• المؤلفون الرئيسيون: Wang, John Chung-Hung, Low, Kin Huat
• مؤلفون آخرون: School of Mechanical and Aerospace Engineering
• التنسيق: مقال
• اللغة: English
• منشور في: 2021
• الموضوعات: Engineering::Aeronautical engineering::Accidents and air safety; Engineering::Aeronautical engineering::Flight simulation; Multirotor; Unmanned Aerial System
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/152326

Pairwise multirotor wake-encounter response studies with identical leader-follower unmanned aerial system (UAS) were conducted for a pair of Phantom 3 sized (∼1.2 kg) multirotor UAS with PX4 attitude controller used on the follower UAS. This is accomplished in the form of one-way coupled wake field...