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Moringa oleifera:A review on nutritive importance and its medicinal application 被引量:40
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作者 Lakshmipriya Gopalakrishnan Kruthi Doriya Devarai Santhosh Kumar 《Food Science and Human Wellness》 SCIE 2016年第2期49-56,共8页
Moringa oleifera,native to India,grows in the tropical and subtropical regions of the world.It is commonly known as‘drumstick tree’or‘horseradish tree’.Moringa can withstand both severe drought and mild frost cond... Moringa oleifera,native to India,grows in the tropical and subtropical regions of the world.It is commonly known as‘drumstick tree’or‘horseradish tree’.Moringa can withstand both severe drought and mild frost conditions and hence widely cultivated across the world.With its high nutritive values,every part of the tree is suitable for either nutritional or commercial purposes.The leaves are rich in minerals,vitamins and other essential phytochemicals.Extracts from the leaves are used to treat malnutrition,augment breast milk in lactating mothers.It is used as potential antioxidant,anticancer,anti-inflammatory,antidiabetic and antimicrobial agent.M.oleifera seed,a natural coagulant is extensively used in water treatment.The scientific effort of this research provides insights on the use of moringa as a cure for diabetes and cancer and fortification of moringa in commercial products.This review explores the use of moringa across disciplines for its medicinal value and deals with cultivation,nutrition,commercial and prominent pharmacological properties of this“Miracle Tree”. 展开更多
关键词 Moringa oleifera Miracle Tree ANTIDIABETIC ANTICANCER COAGULANT
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Rigid body dynamics modeling, experimental characterization, and performance analysis of a howitzer
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作者 Nachiketa TIWARI Mukund PATIL +2 位作者 Ravi SHANKAR Abhishek SARASWAT Rituraj DWIVEDI 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2016年第6期480-489,共10页
A large caliber howitzer is a complex and cumbersome assembly. Understanding its dynamics and performance attributes' sensitivity to changes in its design parameters can be a very time-consuming and expensive exer... A large caliber howitzer is a complex and cumbersome assembly. Understanding its dynamics and performance attributes' sensitivity to changes in its design parameters can be a very time-consuming and expensive exercise, as such an effort requires highly sophisticated test rigs and platforms. However, the need of such an understanding is crucially important for system designers, users, and evaluators. Some of the key performance attributes of such a system are its vertical jump, forward motion, recoil displacement, and force transmitted to ground through tires and trail after the gun has been fired. In this work, we have developed a rigid body dynamics model for a representative howitzer system, and used relatively simple experimental procedures to estimate its principal design parameters. Such procedures can help in obviating the need of expensive experimental rigs, especially in early stages of the design cycle. These parameters were subsequently incorporated into our simulation model,which was then used to predict gun performance. Finally, we conducted several sensitivity studies to understand the influence of changes in various design parameters on system performance. Their results provide useful insights in our understanding of the functioning of the overall system. 展开更多
关键词 HOWITZER GUN CAD modeling Dynamic simulation RECOIL ASSEMBLY PARAMETERS Sensitivity ANALYSIS
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A Novel Sliding-mode Guidance Law Based on Lie-group Method
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作者 韩大鹏 孙未蒙 刘昆 《Defence Technology(防务技术)》 SCIE EI CAS 2010年第1期25-34,共10页
Although the channel-decoupling assumption is often used in design of three-dimensional guidance laws, it loses its rationality for aircrafts with strong kinematics coupling because body rotation arises. To overcome t... Although the channel-decoupling assumption is often used in design of three-dimensional guidance laws, it loses its rationality for aircrafts with strong kinematics coupling because body rotation arises. To overcome this trouble, a novel guiding method was proposed based on Lie-group. After a model of 3D guidance is formulated using vectors, the precision guidance with ending angular constraints can be transformed into a problem involving the relation between directional angles and rotational angular velocities of certain vectors. When the guidance model is imposed a SO(3)-based description, a novel 3D sliding mode guidance law with ending angular constraints can be developed via Lie-group control method and variable structure control theory. Finally, the feasibility and performance of the guidance law were shown by simulating the examples. 展开更多
关键词 control and navigation technology of aircraft multi-constraint guidance Lie group control sliding-mode control
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