Informējam, ka Sistēma pielāgota darbam ar interneta pārlūkprogrammu Internet Explorer (8. un jaunākām versijām) un Mozilla Firefox (3.6 un jaunākām versijām).
Izmantojot citu interneta pārlūkprogrammu, brīdinām, ka Sistēmas funkcionalitāte var tikt traucēta.
<p class="MsoBodyText"><span lang="EN-GB">This document provides a method for evaluating the resonance vibration frequency of the multi-copter unmanned aircraft (UA). This document specifies a method of designing the UA so as to avoid the resonance generated by the coincidence of the natural frequency of the UA body and the rotational frequency of the rotor.</span></p>
<p class="MsoBodyText"><span lang="EN-GB">This document is applicable to multi-copter UA weighing less than 150 kg.</span></p>
Reģistrācijas numurs (WIID)
80801
Darbības sfēra
<p class="MsoBodyText"><span lang="EN-GB">This document provides a method for evaluating the resonance vibration frequency of the multi-copter unmanned aircraft (UA). This document specifies a method of designing the UA so as to avoid the resonance generated by the coincidence of the natural frequency of the UA body and the rotational frequency of the rotor.</span></p>
<p class="MsoBodyText"><span lang="EN-GB">This document is applicable to multi-copter UA weighing less than 150 kg.</span></p>
