This paper is concerned with the attitude control of a three-axis-stabilized spacecraft which consists of a central rigid body and a flexible sun-tracking solar array driven by a solar array drive assembly. Based on t...This paper is concerned with the attitude control of a three-axis-stabilized spacecraft which consists of a central rigid body and a flexible sun-tracking solar array driven by a solar array drive assembly. Based on the linearization of the dynamics of the spacecraft and the modal identi- ties about the flexible and rigid coupling matrices, the spacecraft attitude dynamics is reduced to a formally singular system with periodically varying parameters, which is quite different from a space- craft with fixed appendages. In the framework of the singular control theory, the regularity and impulse-freeness of the singular system is analyzed and then admissible attitude controllers are designed by Lyapunov's method. To improve the robustness against system uncertainties, an H∞ optimal control is designed by optimizing the H∞ norm of the system transfer function matrix. Comparative numerical experiments are performed to verify the theoretical results.展开更多
文摘This paper is concerned with the attitude control of a three-axis-stabilized spacecraft which consists of a central rigid body and a flexible sun-tracking solar array driven by a solar array drive assembly. Based on the linearization of the dynamics of the spacecraft and the modal identi- ties about the flexible and rigid coupling matrices, the spacecraft attitude dynamics is reduced to a formally singular system with periodically varying parameters, which is quite different from a space- craft with fixed appendages. In the framework of the singular control theory, the regularity and impulse-freeness of the singular system is analyzed and then admissible attitude controllers are designed by Lyapunov's method. To improve the robustness against system uncertainties, an H∞ optimal control is designed by optimizing the H∞ norm of the system transfer function matrix. Comparative numerical experiments are performed to verify the theoretical results.
文摘目的探讨无充气腋窝入路腔镜甲状腺手术(endoscopic thyroidectomy by gasless unilateral axillary approach,ETGUA)应用于双侧甲状腺手术的有效性和安全性。方法回顾性匹配研究分析2019年3月至2021年9月浙江省人民医院头颈外科收治的21例进行ETGUA的患者,其中8例为双侧甲状腺癌根治术,13例为单侧甲状腺癌根治术+对侧腺叶切除术(良性)。同时匹配23例行传统颈部切口开放甲状腺手术(conventional open thyroidectomy,COT)的患者作为对照组,其中8例行双侧甲状腺癌根治术,15例单侧甲状腺癌根治术+对侧腺叶切除术(良性),记录ETGUA手术过程,并比较腔镜组与开放组在手术安全性、创伤、术后恢复、患者满意度的差异。以IBM SPSS 25.0软件进行统计分析,Students t测试和χ^(2)检验分析被用来各自分析持续和分类数据。结果手术时长腔镜组(148.67±57.44)min大于开放组(88.48±42.17)min,术后引流量腔镜组大于开放组[(186.52±83.24)ml vs(128.91±116.04)ml,P=0.010],术中出血量[(41.11±43.20)ml vs(29.44±24.55)ml,P=0.796]、术后住院时间[(4.90±0.94)d vs(4.86±1.06)d,P=0.774]、并发症发生率方面差异无统计学意义。腔镜组在术后1 d、1个月及3个月颈部疼痛评分都优于开放组[(2.33±0.91)vs(3.48±1.12),(1.24±0.44)vs(1.70±0.76),(1 vs 1.17±0.39),P=0.001,P<0.032,P<0.048]。在术后美容满意度上,腔镜组优于开放组(1 vs 2.09±0.67,P<0.001)。结论ETGUA是一种安全有效,且美容满意度高的手术方式。