Photosynthetic responses to inorganic carbon in Ulva lactuca under aquatic and aerial states

Intertidal macroalgae experience continual alternation of photosynthesis between aquatic state at high tide and aerial state at low tide. The comparative photosynthetic responses to inorganic carbon were investigated in the common intertidal macroalga Ulva lactuca L. along the coast of Shantou between aquatic and aerial state. The inorganic carbon dissolved in seawater at present could fully (at 10 degreesC or 20 degreesC) or nearly (at 30 degreesC) saturate the aquatic photosynthesis of U. lactuca. However, the aerial photosynthesis was limited by current ambient atmospheric CO2 level, and such a limitation was more severe at higher temperature (20degrees - 30degrees T) than at lower temperature (10 T). The carbon-saturated maximal photosynthesis of U. lactuca under aerial state was much greater than that under aquatic state at 10 degreesC and 20 degreesC, while the maximal photosynthesis under both states was similar at 30 degreesC. The aerial values of K-m (CO2) for photosynthesis were higher than the aquatic values. On the contrary, the values of apparent photosynthetic CO2 conductance under aerial state were considerably lower than that under aquatic state. It was concluded that the increase of atmospheric CO2 would enhance the primary productivity of U. lactuca through stimulating the photosynthesis under aerial state during low tide.

无人机编队飞行技术的研究现状与展望

无人机编队飞行是无人机及其应用技术发展研究的新热点。在分析无人机编队飞行特点的基础上,阐述了无人机编队飞行原理与方法的研究现状,并展望了其今后的主要应用前景。

分布式多无人机编队飞行的阵形保持策略

设计了一种仅采用相对位置偏差状态进行多无人机编队阵形保持的分布式保持策略.首先,分析多无人机编队的特点及其阵形保持问题,提出其阵形保持策略的要求,然后设计一种采用局部阵形状态制定的阵形保持策略.该保持策略从非一致性的冗余状态中进行简洁的处理,判断阵形的保持状态,采取相应的保持机制.最后,应用于几个多无人机编队飞行的例子,仿真结果验证了该保持策略的可行性.

客运架空索道系统动力特性分析方法

客运架空索道系统的固有频率与模态是衡量索道系统固有动力特性的重要指标，固有频率的大小直接关系到结构在各种不同的激励条件下是否会发生动力放大效应与共振。文中首先解决索道系统分析中的有限元建模问题，包括典型柔性索道的模型状态，然后利用ANSYS程序的子空间迭代法求出结构最低各阶的特征值与特征向量，并计算出三种工况下的前40阶固有频率与振动模态，为客运架空索道系统的动力特性分析提供有效的计算方法。

用于阵形控制的无人机编队飞行仿真平台设计与实现

设计了一种模块化结构的无人机编队飞行仿真实验平台.根据阵形控制的模拟需求,将仿真平台进行功能化模块构建,并通过内集方式予以集成.仿真平台结合时序驱动机制、虚拟现实技术、记录与回放技术以及数据分析与重栽软件,使得仿真数据具有时序性、可视性、可记录及重绘性,,操作人员具有高度的参与性,各模拟模块可以根据不同的研究成果进行更改、升级和替代.经过多次仿真实验,该仿真平台运行稳定可靠、占用系统资源小,为无人机编队飞行的研究提供了预验证性的工具,为今后的仿真系统设计提供了一个参考.

用于多无人机编队飞行的PIDA+逆飞行控制器

设计了一种结合PIDA控制及逆控制的多无人机编队飞行控制器.分析了多无人机编队飞行中飞行耦合气流的估计范围,针对个体无人机的轨迹控制模型讨论了其飞行控制器需求,结合逆控制的解耦性能和PIDA控制器低模型依赖、简单结构、快速性等优点,设计了一种PIDA+逆的飞行控制器,最后,以控制器输出约束、飞行气动力参数变化以及气动耦合扰动为指标对PID控制和PIDA+逆控制的控制效果进行了对比仿真,仿真结果表明,PIDA十逆控制能够有效的抑制模型参数不确定性带来的影响,并且在控制器输出约束条件下仍能保持较好的动态性、准确性和鲁棒性.