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561.
Guidance law with impact time and impact angle constraints 总被引:10,自引:8,他引:2
A novel closed-form guidance law with impact time and impact angle constraints is pro- posed for salvo attack of anti-ship missiles, which employs missile’s normal acceleration (not jerk) as the control command directly. Firstly, the impact time control problem is formulated as tracking the designated time-to-go (the difference between the designated impact time and the current flight time) for the actual time-to-go of missile, and the impact angle control problem is formulated as tracking the designated heading angle for the actual heading angle of missile. Secondly, a biased proportional navigation guidance (BPNG) law with designated heading angle constraint is constructed, and the actual time-to-go estimation for this BPNG is derived analytically by solving the system differential equations. Thirdly, by adding a feedback control to this constructed BPNG to eliminate the time-to-go errorthe difference between the standard time-to-go and the actual time-to-go, a guidance law with adjustable coefficients to control the impact time and impact angle simultaneously is developed. Finally, simulation results demonstrate the performance and feasibility of the proposed approach. 相似文献
562.
Simona Proietti Stefano Moscatello Gene A. Giacomelli Alberto Battistelli 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
The effects of the factorial combination of two light intensities (200 and 800 μmol m−2 s−1) and two CO2 concentrations (360 and 800 ppm) were studied on the productivity and nutritional quality of spinach (Spinacia oleracea L.) grown under controlled environment. After 6 weeks within a growth chamber, spinach plants were sampled and analyzed for productivity and quality. There were no statistically significant interactions between the effects of light and CO2 for all of the variables studied, except for the nitrate and oxalic acid content of the leaves. High light and high CO2 independently one from the other, promoted spinach productivity, and the accumulation of ascorbic acid, while their interactive effect limited the accumulation of nitrate and oxalic acid in the spinach leaves. The results highlight the importance of considering the effects of the interaction among environmental variables on maximizing production and the nutritional quality of the food when cultivating and modeling the plant response in controlled environment systems such as for bioregenerative life support. 相似文献
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针对超空泡航行体机动能力差、探测手段有限等特点,提出了一种基于目标舰船尾流梯度信息的变结构制导律.通过激光探测机动目标的尾流信息,动态解算尾流梯度方向;采用滑模变结构理论设计制导律,实现对尾流梯度方向的精确跟踪,最终完成对目标舰船的精确打击.该方法利用目标尾流信息,避免对目标运动状态进行复杂估计计算,不仅降低了对机动能力的要求,同时大大减小能量消耗,提高了有效航程.仿真结果表明,系统响应迅速,可以实现快速精确的目标跟踪打击,且具有很强的鲁棒性和抗干扰性. 相似文献
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文章对国内外航天器热控涂层在轨搭载飞行试验进行了调研,综述了利用和平号空间站、"国际空间站"、美国航天飞机、"长期暴露装置"等航天器进行的相关试验工作及主要的研究成果等。在此基础上提出了我国开展热控涂层搭载飞行试验的建议。 相似文献
566.
Gioia D. Massa Cary A. Mitchell 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Sweetpotato (Ipomea batatas L.) ‘Whatley–Loretan’ was developed for space life support by researchers at Tuskegee University for its highly productive, nutritious storage roots. This promising candidate space life-support crop has a sprawling habit and aggressive growth rate in favorable environments that demands substantial growing area. Shoot pruning is not a viable option for vine control because removal of the main shoot apex drastically inhibits storage-root initiation and development, and chemical growth retardants typically are not cleared for use with food crops. As part of a large effort by the NASA Specialized Center of Research and Training in Advanced Life Support to reduce equivalent system mass (ESM) for food production in space, the dilemma of vine management for sweetpotato was addressed in effort to conserve growth area without compromising root yield. Root yields from unbranched vines trained spirally around wire frames configured either in the shapes of cones or cylinders were similar to those from vines trained horizontally along the bench, but occupying only a small fraction of the bench area. This finding indicates that sweetpotato is highly adaptable to a variety of vine-training architectures. Planting a second plant in the growth container and training the two vines in opposite directions around frames enhanced root yield and number, but had little effect on average length of each vine or bench area occupied. Once again, root yields were similar for both configurations of wire support frames. The 3–4-month crop-production cycles for sweetpotato in the greenhouse spanned all seasons of multiple years during the course of the study, and although electric lighting was used for photoperiod control and to supplement photosynthetic light during low-light seasons, there still were differences in total light available across seasons. Light variations and other environmental differences among experiments in the greenhouse had more effects on vine length than on root yield. Average vine length correlated positively with total hours of daylight received across seasons, and responses for one plant per container were higher above a threshold duration of solar exposure, suggesting that the vines of two plants per container compete for available light. In addition to the adaptability of sweetpotato to various vine-training architectures and across seasons in terms of maintaining root productivity, the open, interior volumes of the support frames tested in this study will provide future opportunity to enhance sweetpotato root yield in space by adding novel interior lighting, such as from intracanopy arrays of light-emitting diodes. This work was sponsored by NASA grant NAG 5 1286. 相似文献
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针对导弹主动防御应用中拦截导弹制导行为辨识问题,提出一种比例导引(PN)制导律多模型辨识滤波方法,对拦截导弹加速度和制导律导航常数进行辨识。采用非线性可观性理论对制导模型的可观性进行了分析。得出在拦截导弹使用PN制导律时,制导模型可观的充要条件。与以往工作相比,该方法考虑了拦截导弹末制导初期由于瞄准误差校正而引起的控制器饱和现象,在拦截导弹执行器处于饱和或退出饱和阶段都能精确对制导律进行辨识。另外,以往工作假定PN制导律常数已知,该方法将PN制导律常数当做制导模型的一个状态进行估计。仿真结果校验了所提方法的性能。 相似文献