Dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing UAV1
Blade upper surface airflow control device and method
Numerical simulation of postlaunching behaviors for a “balloon-borne UAV system”
Dynamics simulation of folding wing UAVs launched from a high-altitude balloon platform
Aerostat inflation measuring device, inflation system and inflation method
Separating structure, parachute pod automatic separating device and application
Aerostat-carried planet sampling return cabin recovery test system
Numerical Evaluation of The Effect of Icing Accretion on An Airship (AIAA 2016-5523)