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Surprises due to new elastoplastic equations of Prandtl-Reuss type
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作者 Heng Xiao Otto Bruhns Albert Meyers 《Acta Mechanica Sinica》 2025年第7期266-291,共26页
New and perhaps unexpected progress in rate-independent elastoplastic modeling is reported with a unified approach toward simulating widely ranging non-elastic effects of various advanced engineering materials such as... New and perhaps unexpected progress in rate-independent elastoplastic modeling is reported with a unified approach toward simulating widely ranging non-elastic effects of various advanced engineering materials such as metals,shape memory alloys,granular materials,fiber-reinforced composites,as well as crystalline solids,etc.This progress originates from a simple idea of bypassing inherent limitations of usual elastoplastic formulations centered on the notion of yielding.With no reference to any yield criteria,the plastic strain-rate should be induced at all stress levels in a more realistic sense that it is small for stresses within a classical yield surface and becomes appreciable for stresses close to and on this surface.A new and unified flow rule for the plastic strain-rate is then proposed of the same smooth form for all cases of both the stress level and the stress rate.Without imposing the ad hoc simplified conditions introduced in usual Prandtl-Reuss equations,new elastoplastic equations are then established by incorporating such small deviations from realistic behaviors as neglected just by postulating these conditions.It turns out that the new equations are not only essentially simpler in both conceptual and structural formulations,but can automatically as inherent response features incorporate significant effects excluded from usual Prandtl-Reuss equations,such as the yielding and unloading behaviors with smooth transitions,the pseudo-elastic effect with hysteresis loops,the non-elastic recovery during unloading as well as failure effects under either monotone or cyclic loading conditions,etc.Since such effects not only go beyond the scope of usual elastoplastic equations but can be only partially simulated even if augmented constitutive equations are postulated toward further characterizing damaging and fracturing effects resulting from evolving micro-defects and macro-cracks,it may be probably surprising that now the new equations of essentially simpler structure not only can in a unified manner simulate all these effects but also can bypass numerical complexities in integrating various rate constitutive equations of complex structures.New results in treating long-standing issues in a few respects are presented,including(i)the yielding and the unloading behaviors with smooth transitions,(ii)the non-elastic recovery during unloading,(iii)the pseudo-elastic effect as extraordinary Bauschinger effect,(iv)failure effects under monotone and cyclic loading,(v)anisotropic multi-mode failure effects of unidirectional composites,(vi)new formulation of crystal elastoplasticity without involving non-uniqueness and singularity issues,(vii)non-normality effects for non-proportional multi-axial loading cases,and(viii)high efficiency algorithms for simulating multi-axial fatigue effects. 展开更多
关键词 ELASTOPLASTIC All-through dissipation Smooth transition Failure Non-elastic recovery PSEUDO-ELASTICITY ANISOTROPY Crystalline slip Non-proportional loading high-efficiency algorithm
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某型反坦克导弹的高原适应性改造 被引量:1
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作者 刘海亮 黄大山 +2 位作者 王炳奇 罗德智 张文杨 《兵器装备工程学报》 CAS 北大核心 2020年第S02期197-200,共4页
为解决某型反坦克导弹在高原试射过程中出现发射后掉落的问题,采用了增添反馈回路,引入陀螺仪、加速度感应装置,加入EMPC自动驾驶仪的方法。与无校正、变系数法校正、EMPC方法校正相比,高效EMPC方法超调量小、调整时间短,动态特性提升... 为解决某型反坦克导弹在高原试射过程中出现发射后掉落的问题,采用了增添反馈回路,引入陀螺仪、加速度感应装置,加入EMPC自动驾驶仪的方法。与无校正、变系数法校正、EMPC方法校正相比,高效EMPC方法超调量小、调整时间短,动态特性提升较为明显。从调节速度、适用性等方面论证了高效EMPC高原适应性改造方案的可行性和优越性。 展开更多
关键词 反坦克导弹 高效empc算法 显式模型预测控制 变系数网络校正法 高原适应性改造
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剥离饱和区域的高效显式模型预测控制算法 被引量:1
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作者 刘海亮 马飞越 +1 位作者 佃松宜 孔令尧 《电光与控制》 CSCD 北大核心 2019年第9期60-65,共6页
在复杂快速多维度约束系统中,针对在显式模型预测控制离线计算时,计算量大、处理缓慢、内存占用过高等问题,提出了一种基于剥离饱和区域的高效显式模型预测控制算法。结合多面体、分段仿射等相关概念和波利亚定理,利用显式控制器反馈饱... 在复杂快速多维度约束系统中,针对在显式模型预测控制离线计算时,计算量大、处理缓慢、内存占用过高等问题,提出了一种基于剥离饱和区域的高效显式模型预测控制算法。结合多面体、分段仿射等相关概念和波利亚定理,利用显式控制器反馈饱和特性,去除饱和区域,保留非饱和临界区域,从而达到减少状态分区数量和计算量的目的。根据解耦后四旋翼飞行器的两个状态空间子系统简化模型,实现了姿态角在扰动后的快速准确调节。数值仿真和半实物仿真实验均验证了该算法在四旋翼飞行器姿态控制上的有效性和优越性。 展开更多
关键词 四旋翼飞行器 高效empc算法 显式模型预测控制 状态分区 分段仿射 波利亚阶数
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