皮卫星具有成本低、反应灵敏等特点,是航天领域的研究热点。由于体积和质量的限制,大卫星复杂的星载计算机系统结构并不适用于皮卫星。介绍基于COTS器件的皮卫星星载计算机系统模块化设计技术,将多准则决策方法 TOPSIS排序法应用于皮卫...皮卫星具有成本低、反应灵敏等特点,是航天领域的研究热点。由于体积和质量的限制,大卫星复杂的星载计算机系统结构并不适用于皮卫星。介绍基于COTS器件的皮卫星星载计算机系统模块化设计技术,将多准则决策方法 TOPSIS排序法应用于皮卫星的芯片选型。研制2版基于不同低功耗微控制单元的计算机原理样机,并通过大量实验测试比较2版原理样机的速度、功耗、运行温度等性能。当工作温度为27℃,主频为8 MHz时,基于MSP430芯片和ATxmega芯片的原理样机的MIPS值分别为7.449和6.781;运行加法运算的时间分别为0.613μs和1.381μs,功耗分别为38.224 m W和54.411 m W。在-40℃-85℃时,原理样机均可正常工作。展开更多
The stress rate integral equations of elastoplasticity are deduced based on Ref. [1] by consistent methods. The point at which the stresses and/or displacements are calculated can be in the body or on the boundary, an...The stress rate integral equations of elastoplasticity are deduced based on Ref. [1] by consistent methods. The point at which the stresses and/or displacements are calculated can be in the body or on the boundary, and in the plastic region or elastic one. The existence of the principal value integral in the plastic region is demonstrated strictly, and the theoretical basis is presented for the paticular solution method by unit initial stress fields. In the present method, programming is easy and general, and the numerical results are excellent.展开更多
文摘皮卫星具有成本低、反应灵敏等特点,是航天领域的研究热点。由于体积和质量的限制,大卫星复杂的星载计算机系统结构并不适用于皮卫星。介绍基于COTS器件的皮卫星星载计算机系统模块化设计技术,将多准则决策方法 TOPSIS排序法应用于皮卫星的芯片选型。研制2版基于不同低功耗微控制单元的计算机原理样机,并通过大量实验测试比较2版原理样机的速度、功耗、运行温度等性能。当工作温度为27℃,主频为8 MHz时,基于MSP430芯片和ATxmega芯片的原理样机的MIPS值分别为7.449和6.781;运行加法运算的时间分别为0.613μs和1.381μs,功耗分别为38.224 m W和54.411 m W。在-40℃-85℃时,原理样机均可正常工作。
基金The project supported by the National Natural Science Foundation of China
文摘The stress rate integral equations of elastoplasticity are deduced based on Ref. [1] by consistent methods. The point at which the stresses and/or displacements are calculated can be in the body or on the boundary, and in the plastic region or elastic one. The existence of the principal value integral in the plastic region is demonstrated strictly, and the theoretical basis is presented for the paticular solution method by unit initial stress fields. In the present method, programming is easy and general, and the numerical results are excellent.