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Ehsan Taheri Ilya Kolmanovsky Ella Atkins 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(3):879-890
Shape-based methods are becoming popular in low-thrust trajectory optimization due to their fast computation speeds. In existing shape-based methods constraints are treated at the acceleration level but not at the thrust level. These two constraint types are not equivalent since spacecraft mass decreases over time as fuel is expended. This paper develops a shape-based method based on a Fourier series approximation that is capable of representing trajectories defined in spherical coordinates and that enforces thrust constraints. An objective function can be incorporated to minimize overall mission cost, i.e., achieve minimum . A representative mission from Earth to Mars is studied. The proposed Fourier series technique is demonstrated capable of generating feasible and near-optimal trajectories. These attributes can facilitate future low-thrust mission designs where different trajectory alternatives must be rapidly constructed and evaluated. 相似文献
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Shtessel Yuri B. Shkolnikov Ilya A. Levant Arie 《IEEE transactions on aerospace and electronic systems》2009,45(1):110-124
A new smooth second-order sliding mode control (SSOSM) is proposed and proved for a system driven by uncertain sufficiently smooth disturbances. The main target application of this technique, the missile interceptor guidance-control system against targets performing evasive maneuvers, is considered to demonstrate benefits of this design for a two-loop integration of guidance and flight control systems. The designed guidance-control system performance is verified via computer simulations using a miniature hypervelocity kinetic energy endo-atmospheric interceptor planar model. 相似文献
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Elizaveta E. Antonova Ilya L. Ovchinnikov 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2001,28(12):1747-1752
Theory of the plasma sheet with medium-scale developed turbulence gives the possibility to explain the main processes of plasma sheet bifurcation and theta-aurora formation during IMF Bz > 0. The model suggests that during IMF Bz > 0 small bulge structure in the plasma sheet center is formed. The polarization of the bulge due to dawnward electron motion and duskward ion motion decreases the large-scale electric field in the bulge region. The decrease of the large-scale field in the conditions of constant coefficient of diffusion leads to the bulge growth. The results of plasma sheet bifurcation and theta-aurora formation modelling are presented. 相似文献
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在非结构网格上求解非线性航空声学问题的高精度有限体积法 总被引:1,自引:0,他引:1
Ilya ABALAKIN Alain DERVIEUX Tatiana KOZUBSKAYA 《中国航空学报》2006,19(2):97-104
介绍了有限体积数值方法,该方法适用于在任意非结构网格上求解线性和非线性的航空声学问题.本方法基于角点-中心的多参数格式,可在笛卡尔网格上达到六阶精度,对于可能的不连续性采用了自适应耗散.通过一系列算例研究了该方法的特性,结果表明:在模拟谐振型管中的噪声抑制中,所提出的方法是很有效的. 相似文献
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Sofya A. Ushakova Alexander A. Tikhomirov Valentin N. Shikhov Jean-Bernard Gros Tamara K. Golovko Igor V. Dal’ke Ilya G. Zakhozhii 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
The main objective of a life support system for space missions is to supply a crew with food, water and oxygen, and to eliminate their wastes. The ultimate goal is to achieve the highest degree of closure of the system using controlled processes offering a high level of reliability and flexibility. Enhancement of closure of a biological life support system (BLSS) that includes plants relies on increased regeneration of plant waste, and utilization of solid and liquid human wastes. Clearly, the robustness of a BLSS subjected to stress will be substantially determined by the robustness of the plant components of the phototrophic unit. The aim of the present work was to estimate the heat resistance of two plants (wheat and lettuce) grown on human wastes. Human exometabolites mineralized by hydrogen peroxide in an electromagnetic field were used to make a nutrient solution for the plants. We looked for a possible increase in the heat tolerance of the wheat plants using changes in photosynthetically active radiation (PAR) intensity during heat stress. At age 15 days, plants were subjected to a rise in air temperature (from 23 ± 1 °C to 44 ± 1 °С) under different PAR intensities for 4 h. The status of the photosynthetic apparatus of the plants was assessed by external СО2 gas exchange and fluorescence measurements. The increased irradiance of the plants during the high temperature period demonstrated its protective action for both the photosynthetic apparatus of the leaves and subsequent plant growth and development. The productivity of the plants subjected to temperature changes at 250 W m−2 of PAR did not differ from that of controls, whereas the productivity of the plants subjected to the same heat stress but in darkness was halved. 相似文献
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Biswas Akash Karak Bidya Binay Usoskin Ilya Weisshaar Eckhard 《Space Science Reviews》2023,219(3):1-70
Space Science Reviews - The InSight lander carried an Instrument Deployment System (IDS) that included an Instrument Deployment Arm (IDA), scoop, five finger “claw” grapple,... 相似文献
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