PRISE 发表于 2025-3-26 21:20:08
http://reply.papertrans.cn/59/5861/586094/586094_31.pngencyclopedia 发表于 2025-3-27 01:45:12
http://reply.papertrans.cn/59/5861/586094/586094_32.png小步走路 发表于 2025-3-27 06:58:11
http://reply.papertrans.cn/59/5861/586094/586094_33.pngopportune 发表于 2025-3-27 12:58:24
The Concepts of Telescopic and Self-Deployable Tensegrity-Based Helium-Filled Aerostats,tat volume and shape during the flight, which results in the possibility of vertical motion control. The first proposed construction is telescopic aerostat with multi-segmented construction and controllable segments’ couplings. In turn, the second construction is based on a self-deployable tensegrit易受骗 发表于 2025-3-27 15:31:55
http://reply.papertrans.cn/59/5861/586094/586094_35.pngAlbinism 发表于 2025-3-27 18:50:55
Designing Helium-Filled Aerostats Applying Scaling Procedure, Mini-Models CANDY and Fly-Tests on SK, helium can be pumped into the aerostat (using storage tank with a compressed gas), starting its autonomous mission. Optimal design process of aerostats dedicated to perform determined mission (between the altitudes . and .) will be discussed with preliminary experimental verification process, base很是迷惑 发表于 2025-3-28 00:25:24
http://reply.papertrans.cn/59/5861/586094/586094_37.pngthyroid-hormone 发表于 2025-3-28 04:42:49
http://reply.papertrans.cn/59/5861/586094/586094_38.png浪荡子 发表于 2025-3-28 07:52:22
Numerical Approach to Maneuver Design and Feasibility Evaluation for the Autonomy of Airship,roposed maneuvers. This paper demonstrates a holistic approach to maneuver design by emphasizing its feasibility with consideration on the complete dynamics of the system and its constraints. Computational bifurcation analysis is employed to generate a sequence of trim solutions based on specified scartilage 发表于 2025-3-28 10:53:43
,Estimation of Stability Derivatives Due to Translational Motion of Various LTA Vehicles Using CFD,derivatives due to the translational motion of the aerostat are considered for the analysis in this paper. The extraction of the stability derivatives involves the simulation of the oscillations of the aerostat along the vertical direction (heave motion) and axial direction (surge motion). A forced