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1)  reference trajectory estimation
参考轨迹估计
2)  reference path
参考轨迹
1.
Adopting predictive function control to calculate control instructions and applying fuzzy inference to compensate the controlled quantity make fighter track the planned optimal reference path automatically, plenty of numeral simulation referring to various typical terrain show that the scheme is feasible.
为了获得简单而又精密的控制器,采用预测函数控制计算控制指令,并运用模糊推理对控制量进行补偿,设计出合理的预测轨迹控制系统,使飞机自动地跟踪已规划出的最优参考轨迹,并针对各种典型地形进行了数字仿真,大量的数字仿真表明该方案是可行的。
2.
Adopting predictive function control to calculate control instructions and applying fuzzy inference to compensate the controlled quantity make fighter tracks the planned optimal reference path automatically.
采用预测函数控制计算控制指令,并运用模糊推理对控制量进行补偿,使飞机自动地跟踪已规划出的最优参考轨迹,并针对各种典型地形进行了数字仿真,大量的数字仿真表明该方案符合地形跟随系统的要求。
3)  reference trajectory
参考轨迹
1.
Self-tuning scheme of predictive function control s reference trajectory based on expected response;
基于期望响应的预测函数控制参考轨迹自校正方法
2.
By utilizing the constraints of internally stability and asyptotically tracking the reference trajectory that satisfies the basic specifications was constructed and a new algorithm was developed for the process.
该算法通过求取满足闭环系统最基本要求的参考轨迹来实现 。
3.
According to sensitivity to initial value in reentry trajectory optimization for hypersonic glide vehicles with multi-constraints,this paper develops a rapid reference trajectory planning methodology.
针对多约束的高超声速滑翔飞行器的再入轨迹优化时对初值敏感的问题,提出一种参考轨迹快速规划算法。
4)  reference locus
参考轨迹
1.
After defining the min robust index, we discussed the effect of the reference locus, and further, we brought forward a method of designing the reference locus, it s based on the designing of the reference locus of set value and interaction relapsing.
在定义最小鲁棒指数的基础上 ,分析了参考轨迹对系统鲁棒性的影响以及当前参考轨迹的缺陷 ,提出了基于设定值跟踪参考轨迹和扰动回复参考轨迹叠加的新的参考轨迹设计方法。
5)  reference trajectory coefficient
参考轨迹系数
6)  sliding mode reference trajectory
滑模参考轨迹
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