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基于栈结构的浮点型数据表达式求值算法 总被引:1,自引:0,他引:1
表达式求值是程序设计语言编译中的一个基本问题,任何程序设计语言都涉及到了表达式求值的功能,对于按常规输入即中缀表达式输入格式的表达式求值问题不但要进行整型数据的运算,而且更重要的是浮点型数据的运算。 相似文献
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将全球卫星定位系统(GPS)单历元的L1波段的载波相位和码相位观测方程进行组合求解整周模糊度的浮点解。基于对浮点解与固定解间关系的分析,提出了一种将低精度浮点解映射到固定解的方法,降低了最小二乘降相关平差(LAMBDA)算法对高精度浮点解的依赖性,避免了多个历元求解高精度浮点解,实现了单频、单历元的整周模糊度估计。实际数据测试结果表明:算法的成功率大于95%,能有效地实时解算动态姿态。 相似文献
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Xin-Lin Xia De-Fu Li Chuang Sun Li-Ming Ruan 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
The prediction of the thermal behavior of stratospheric balloons under varying environmental conditions is one of the key issues in the design and flight test of balloons. In this paper, a three-dimensional transient thermal model is developed to predict the thermal behavior of spherical stratospheric balloons. The diurnal variations of the skin and lifting gas temperatures at float conditions are discussed in detail. The further studies on the thermal behavior of stratospheric balloons are presented also. 相似文献
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《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(5):1375-1382
When a stratospheric airship free floats at pressure altitude, the sideslip angle of the airship is neither random nor against the wind, but is stable on certain values. According to classical potential flow theory, a simplified two-dimensional ellipse and three-dimensional ellipsoid are firstly analyzed respectively, which implied that the airship could present crosswind orientation. The numerical investigations (CFD) on the yaw stability based on a bare hull and a finned airship are employed for verifying the theory conclusion. It is found that the finned airships can remain stable when its sideslip Angle is 55–70°, which is less than 90° of the stable angle of the ellipsoid and bare hull, but statically unstable at low sideslip angles, its static instability is similar to that of dynamic flight. Then the fight data of three stratospheric airships is analyzed. The yaw stability in flight data generally agrees with expectations drawn of theoretical and numerical simulation. These investigations serve to provide references for yaw control and configuration design of airships. 相似文献
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本文提出了一种结合浮点数编码和格雷码编码的混合编码遗传算法。该算法有机结合了浮点数编码和格雷码编码的优点,不易陷入早熟收敛且局部搜索能力强,收敛速度快。本文对一系列典型函数进行了优化计算,试验结果证实了这种混合编码遗传算法的有效性和优越性能。 相似文献
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Xiaojian Li Xiande FangQiuming Dai Zhanru Zhou 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
In recent years, the study of semi-rigid airship has revived with the development of airships. Semi-rigid airships have some characteristics of rigid airships and non-rigid airships. Due to the flexibility of the envelope of the non-rigid airship, the variation of the temperature of the inner gas will lead to its structure deformation and affect its flight altitude. This paper develops the structural mechanics model, thermodynamic model and dynamic model of the semi-rigid airship, based on which nonlinear finite element analysis is employed for geometrically nonlinear deformation of the airship upper film in consideration of thermodynamics and structural mechanics coupling. Based on the thermal-structural interaction, the thermal characteristics and flight performances of the airship during floating flight are investigated. The 3-D solar radiation and temperature distribution of the airship skin and the temperature variation of the inner gas are presented to investigate the thermal performance of the airship, flight velocity, acceleration and flight altitude are simulated to investigate the flight performance, and the variations of the volume and pressure difference of the inner gas are calculated to provide a basis for structure design. The results of the simulation can be referenced for the design of the semi-rigid airship, and can be used for the further study on the attitude control of the airship during its floating flight. 相似文献
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