Development of a hardware-in-the-loop simulator and flight simulation of a subscale experimental winged rocket
Development of a hardware-in-the-loop simulator and flight simulation of a subscale experimental winged rocket
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DOI：
10.1109/aim.2013.6584309
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发表时间：
2013-07
期刊：
影响因子：
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通讯作者：
H. Yamasaki;Takaaki Matsumoto;Kyoshiro Itakura;S. Miyamoto;K. Yonemoto
中科院分区：
文献类型：
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作者：
H. Yamasaki;Takaaki Matsumoto;Kyoshiro Itakura;S. Miyamoto;K. Yonemoto
本文介绍了一个半实物仿真器的开发和飞行仿真的缩比实验有翼火箭。为评估有翼火箭的性能，研制了半实物仿真器。利用半实物仿真器研究了上升段和返回段的两种控制策略。仿真结果表明，采用两种策略，火箭都能安全上升和返回。然而，结果也表明，在上升阶段，迎角和俯仰角都应该用于升降舵控制，因为这会产生很高的最大高度。WIRES#014将于2013年进行飞行试验，并将硬件在环仿真结果与真实的飞行数据进行比较。
This paper addresses the development of a hardware-in-the-loop simulator and flight simulation of a subscale experimental winged rocket. The hardware-in-the-loop simulator was developed to evaluate the performance of the winged rocket. Two control strategies for the ascent and return flights were studied using the hardware-in-the-loop simulator. The simulation results showed that the rocket can safely ascend and return using both strategies. However, the results also indicated that both the angle of attack and pitch angle should be used for elevator control during the ascent phase as this produces a high maximum altitude. A flight test of WIRES#014 will be conducted in 2013, and the hardware-in-the-loop simulation results will be compared with real flight data.