Abstract
Dielectric elastomers (DEs) are lightweight and high-power, making them ideal for power control in a planetary exploration spacecraft. In this chapter, we will discuss the control of an exploration airplane exploring the surface of Mars using DEs. This airplane requires lightweight and powerful actuators to fly in the rare Martian atmosphere. DEs are a possible candidate for use as actuator controlling the airplane since they have high power, and high efficiency. A structural model of a wing having a control surface, a DE, and a linkage was built and a wind tunnel test of a control surface actuation using a DE actuator was carried out.
Reference34 articles.
1. Nagai H, Oyama A: Mars Airplane, W.G. (2013) Mission Scenario of Mars Exploration by Airplane. Proceedings of the 2013 Asia-Pacific International Symposium on Aerospace Technology. 2013; 8:1-3.
2. Fujita K, Luong R, Nagai H, Asai K: Conceptual Design of Mars Airplane, Trans. JSASS Aerospace Tech. Japan. 2012; 10: 28p.
3. Fujita K, Nagai H, Robustness Analysis on Aerial Deployment Motion of a Mars Airplane using Multibody Dynamics Simulation: Effects of Wing-Unfolding Torque and Timing, The Aeronautical Journal. 2017; 121,1238: 449-468, DOI: 10.1017/aer.2016.123.
4. Fujita K, Chiba S et al, Feasibility of artificial muscle for mars airplane. Aeron Aero Open Access J: 2018; 111: p213, DOI:10.15406/aaoaj.2018.02.00052.
5. Fujita K, Oyama O, Kubo D, Kanazaki M, Nagai H, Wind Tunnel Test for Videogrammetric Deformation Measurement of UAV for Mars Airplane Balloon Experiment-1 (MABE-1), Journal of Flow Control, Measurement & Visualization. 2019; 7:87-100, DOI: 10.4236/jfcmv.2019.72007
Cited by
4 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献