valid states are 'starting running'. the machine is in the 'poweroff' state 的解决

最新推荐文章于 2023-04-24 16:43:03 发布
原创 最新推荐文章于 2023-04-24 16:43:03 发布 · 1.8k 阅读 · 0 ·
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#centos #bios #虚拟化

本文提供了解决 CentOS6.5 系统在使用 VirtualBox 和 Vagrant 启动时出现的错误：'validstatesare'startingrunning',themachineisinthe'poweroff'state'的方法。通过设置 BIOS 中的 Intel VT 来解决该问题，并提供了其他可能的解决方案链接。

CentOS 6.5 ， 装 VBox4.3 ， vagrant 1.6.5 ， Panamax  ，启动时报错：

valid states are 'starting running'. the machine is in the 'poweroff' state

解决方法： 设置 Intel VT ：  

开机进BIOS（thinkpad 240  F1键 ）： 

 Security  --Virtualization --Intel Virtualization Technology    --------Enabled
重启系统， 已无此报错，如果没有决绝，参考尝试这里的其他方式：
https://github.com/mitchellh/vagrant/issues/2157

（其他报错，解决中）

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用命令行vagrant up启动时报错： Valid states are 'starting, running'. The machine is in the 'poweroff' state. 接着尝试使用VBox启动，报错如下：
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HP部分笔记本，重写BIOS或更换主板后，开机提示“WANING!!-Machine is not in committedstate！”屏幕出现"主机处于未定义状态"警告。如下图：这个报错是由于未对主板的AMT功能进行定义造成的。主板备件的AMT功能处于未定义状态，而新的BIOS增加了检测主板是否被正确定义的功能并相应在启动时给出提示。查看掌托上的IntelCPU标签，如果带有vpro字样，则...
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当存储数据时，有时会报错，说存储不成功，到底是什么原因呢？     在存储数据时，往往有一个保存类型的选择，当为shapefile时，必须存储在文件夹中，而当选择其他数据类型时必须创建数据库或选择已用数据库，大家出现错误的很多时候都是因为选择不匹配，但是小编还是建议大家将数据存储在数据库中，习惯数据库的存储模式，因为数据库对数据的要求低，一般情况下不会有错，也方便大家的管理。    
imx-snvs-poweroff.rar_The First_imx
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【标题】"imx-snvs-poweroff.rar_The First_imx" 涉及的是针对i.MX（Image Media eXtension）处理器系列的SNVS（Secure Non-Volatile Storage Subsystem）模块的电源管理驱动程序的第一个版本。i.MX处理器是恩智浦...
function [state1, state2] = m_fnShiXu(state) % 时序函数，提供起飞、级间分离与点火的判据 % 确保state是结构体 if ~isstruct(state) error('state必须是结构体'); end % 确保const子结构体存在 if ~isfield(state, 'const') || ~isstruct(state.const) state.const = struct(); end % 确保dhconst字段存在 if ~isfield(state.const, 'dhconst') state.const.dhconst = 0.01; % 设置默认值 end dh = state.const.dhconst; % 现在安全访问 % 初始化阶段标志和文件指针 state.fpCombined = -1; % 初始化为无效文件标识符 state.fpCombined1 = -1; % 初始化为无效文件标识符 % 载入（气动）参数 state = m_fnLoadData(); state.const.Flag_write=1; % 存储（弹道）参数 if state.const.Flag_write % 设置输出数据的保存位置 outputDir = './OUTPUT/'; % 确保输出目录存在 if ~exist(outputDir, 'dir') mkdir(outputDir); end % 尝试打开文件 state.fpCombined = fopen(fullfile(outputDir, 'CombinedData.csv'), 'w'); if state.fpCombined == -1 error('无法打开文件 CombinedData.csv'); end state.fpCombined1 = fopen(fullfile(outputDir, 'LamdaBWeiHeight.csv'), 'w'); if state.fpCombined1 == -1 fclose(state.fpCombined); % 关闭已打开的文件 error('无法打开文件 LamdaBWeiHeight.csv'); end % 写入CSV表头 fprintf(state.fpCombined, 'x0[1],x0[2],x0[3],x0[4],x0[5],x0[6],x0[7],phi*RTD,psi*RTD,gamma*RTD,theta*RTD,sigma*RTD,alpha*RTD,beta*RTD,Height,Vnorm,ma,MassRoc,thetaK*RTD,q,F_Engine[1],Lamda*RTD,BWei*RTD,Range,dW22[1],dW22[2],dW22[3],g[1],g[2],g[3],P*101.325,T,midu,p_mathpri.OrElement[1],p_mathpri.OrElement[2],p_mathpri.OrElement[3]*RTD,p_mathpri.OrElement[4]*RTD,p_mathpri.OrElement[1]*(1+p_mathpri.OrElement[2])-6378,p_mathpri.OrElement[1]*(1-p_mathpri.OrElement[2])-6378,nx,nz\n'); end const= init_rocket_state(); % ==================================================================== % 一级发动机工作阶段 % ==================================================================== state.TimeLeft = const.TimeP1; state.Flag_PowerOff = 0; state.phase = 1; state.iflag = 0; step = 1; while ~state.Flag_PowerOff if state.iflag ~= 0 state.TimeLeft = state.TimeLeft -state.dh; end if (state.TimeLeft < state.dh) && (abs(state.TimeLeft - state.dh) > state.const.ErrorTime) state.dh = state.TimeLeft; end % 执行龙格-库塔法积分 state.x0 = m_fnRK(state.x0, state.dh); % 调用动态计算函数获取所有参数 [state, dx] = m_fnDynamic(state,const); if state.Flag_write % 存储结果 state.results(step, :) = [state.x0(1), state.x0(2), state.x0(3), state.x0(4), state.x0(5), state.x0(6), state.x0(7), ... state.phi*state.const.RTD, state.psi*state.const.RTD, state.gamma*state.const.RTD, ... state.theta*state.const.RTD, state.sigma*state.const.RTD, state.alpha*state.const.RTD, ... state.beta*state.const.RTD, state.Height, state.Vnorm, state.ma, state.MassRoc, ... state.thetaK*state.const.RTD, state.q, state.F_Engine(1), state.Lamda*state.const.RTD, ... state.BWei*state.const.RTD, state.Range, state.dW22(1), state.dW22(2), state.dW22(3), ... state.g(1), state.g(2), state.g(3), state.P*101.325, state.T, state.midu, ... state.OrElement(1), state.OrElement(2), state.OrElement(3)*state.const.RTD, ... state.OrElement(4)*state.const.RTD, state.OrElement(1)*(1+state.OrElement(2))-6378, ... state.OrElement(1)*(1-state.OrElement(2))-6378, state.nx, state.nz]; % 写入LamdaBWeiHeight文件 fprintf(state.fpCombined1, '%10.12f,%10.12f,%10.12f\n', state.Height, state.Lamda*state.const.RTD, state.BWei*state.const.RTD); end % 检查是否到达关机时间 if abs(state.TimeLeft - state.dh) < state.const.ErrorTime state.Flag_PowerOff = 1; end state.iflag = state.iflag + 1; step = step + 1; end % 保存一级关机时刻的状态 state1 = [state.x0(1), state.x0(2), state.x0(3), state.x0(4), state.x0(5), state.x0(6), state.x0(7), state.phase]; % 输出关键参数到控制台 fprintf(' 时间（s） 高度（m） 绝对速度（m/s） 当地弹道倾角（°） 攻角（°） 俯仰角（°）\n'); fprintf(' 一级关机：%f %f %f %f %f %f\n', ... state.x0(1), state.Height, state.VEInorm, state.thetaK*state.const.RTD, state.alpha*state.const.RTD, state.phi*state.const.RTD); % ==================================================================== % 滑翔1阶段 % ==================================================================== state.phase = 2; state.TimeLeft = state.const.TimeH1; state.Flag_PowerOff = 0; state.iflag = 0; while ~state.Flag_PowerOff if state.iflag ~= 0 state.TimeLeft = state.TimeLeft - state.dh; end if (state.TimeLeft < state.dh) && (abs(state.TimeLeft - state.dh) > state.const.ErrorTime) state.dh = state.TimeLeft; end % 执行龙格-库塔法积分 state.x0 = m_fnRK(state.x0, state.dh); % 调用动态计算函数获取所有参数 [state, dx] = m_fnDynamic(state); if state.Flag_write % 写入CombinedData文件 fprintf(state.fpCombined, '%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f\n', ... state.x0(1), state.x0(2), state.x0(3), state.x0(4), state.x0(5), state.x0(6), state.x0(7), ... state.phi*state.const.RTD, state.psi*state.const.RTD, state.gamma*state.const.RTD, ... state.theta*state.const.RTD, state.sigma*state.const.RTD, state.alpha*state.const.RTD, ... state.beta*state.const.RTD, state.Height, state.Vnorm, state.ma, state.MassRoc, ... state.thetaK*state.const.RTD, state.q, state.F_Engine(1), state.Lamda*state.const.RTD, ... state.BWei*state.const.RTD, state.Range, state.dW22(1), state.dW22(2), state.dW22(3), ... state.g(1), state.g(2), state.g(3), state.P*101.325, state.T, state.midu, ... state.OrElement(1), state.OrElement(2), state.OrElement(3)*state.const.RTD, ... state.OrElement(4)*state.const.RTD, state.OrElement(1)*(1+state.OrElement(2))-6378, ... state.OrElement(1)*(1-state.OrElement(2))-6378, state.nx, state.nz); % 写入LamdaBWeiHeight文件 fprintf(state.fpCombined1, '%10.12f,%10.12f,%10.12f\n', state.Height, state.Lamda*state.const.RTD, state.BWei*state.const.RTD); end % 检查是否到达关机时间 if abs(state.TimeLeft - state.dh) < state.const.ErrorTime state.Flag_PowerOff = 1; end state.iflag = state.iflag + 1; end fprintf('滑翔第一次：%f %f %f %f %f %f\n', ... state.x0(1), state.Height, state.VEInorm, state.thetaK*state.const.RTD, state.alpha*state.const.RTD, state.phi*state.const.RTD); % ==================================================================== % 二级第一次开机 % ==================================================================== state.phase = 3; state.TimeLeft = state.const.TimeP21; state.Flag_PowerOff = 0; state.iflag = 0; % 初始化状态保存变量 state2 = zeros(8, 1); state.bFirstCapture = true; % 用于记录是否已捕获110km高度状态 while ~state.Flag_PowerOff if state.iflag ~= 0 state.TimeLeft = state.TimeLeft - state.dh; end if (state.TimeLeft < state.dh) && (abs(state.TimeLeft - state.dh) > state.const.ErrorTime) state.dh = state.TimeLeft; end % 执行龙格-库塔法积分 state.x0 = m_fnRK(state.x0, state.dh); % 调用动态计算函数获取所有参数 [state, dx] = m_fnDynamic(state); if state.Flag_write % 写入CombinedData文件 fprintf(state.fpCombined, '%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f\n', ... state.x0(1), state.x0(2), state.x0(3), state.x0(4), state.x0(5), state.x0(6), state.x0(7), ... state.phi*state.const.RTD, state.psi*state.const.RTD, state.gamma*state.const.RTD, ... state.theta*state.const.RTD, state.sigma*state.const.RTD, state.alpha*state.const.RTD, ... state.beta*state.const.RTD, state.Height, state.Vnorm, state.ma, state.MassRoc, ... state.thetaK*state.const.RTD, state.q, state.F_Engine(1), state.Lamda*state.const.RTD, ... state.BWei*state.const.RTD, state.Range, state.dW22(1), state.dW22(2), state.dW22(3), ... state.g(1), state.g(2), state.g(3), state.P*101.325, state.T, state.midu, ... state.OrElement(1), state.OrElement(2), state.OrElement(3)*state.const.RTD, ... state.OrElement(4)*state.const.RTD, state.OrElement(1)*(1+state.OrElement(2))-6378, ... state.OrElement(1)*(1-state.OrElement(2))-6378, state.nx, state.nz); % 写入LamdaBWeiHeight文件 fprintf(state.fpCombined1, '%10.12f,%10.12f,%10.12f\n', state.Height, state.Lamda*state.const.RTD, state.BWei*state.const.RTD); end % 检查是否到达关机时间 if abs(state.TimeLeft - state.dh) < state.const.ErrorTime state.Flag_PowerOff = 1; end % 捕获110km高度状态 if (state.Height / 1000 >= 110) && state.bFirstCapture state2(1:7) = state.x0; state2(8) = state.phase; state.bFirstCapture = false; end state.iflag = state.iflag + 1; end fprintf('二级一次关机：%f %f %f %f %f %f\n', ... state.x0(1), state.Height, state.VEInorm, state.thetaK*state.const.RTD, state.alpha*state.const.RTD, state.phi*state.const.RTD); % ==================================================================== % 滑翔2阶段 % ==================================================================== state.phase = 4; state.TimeLeft = state.const.TimeH2; state.Flag_PowerOff = 0; state.iflag = 0; while ~state.Flag_PowerOff if state.iflag ~= 0 state.TimeLeft = state.TimeLeft - state.dh; end if (state.TimeLeft < state.dh) && (abs(state.TimeLeft - state.dh) > state.const.ErrorTime) state.dh = state.TimeLeft; end % 执行龙格-库塔法积分 state.x0 = m_fnRK(state.x0, state.dh); % 调用动态计算函数获取所有参数 [state, dx] = m_fnDynamic(state); if state.Flag_write % 写入CombinedData文件 fprintf(state.fpCombined, '%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f\n', ... state.x0(1), state.x0(2), state.x0(3), state.x0(4), state.x0(5), state.x0(6), state.x0(7), ... state.phi*state.const.RTD, state.psi*state.const.RTD, state.gamma*state.const.RTD, ... state.theta*state.const.RTD, state.sigma*state.const.RTD, state.alpha*state.const.RTD, ... state.beta*state.const.RTD, state.Height, state.Vnorm, state.ma, state.MassRoc, ... state.thetaK*state.const.RTD, state.q, state.F_Engine(1), state.Lamda*state.const.RTD, ... state.BWei*state.const.RTD, state.Range, state.dW22(1), state.dW22(2), state.dW22(3), ... state.g(1), state.g(2), state.g(3), state.P*101.325, state.T, state.midu, ... state.OrElement(1), state.OrElement(2), state.OrElement(3)*state.const.RTD, ... state.OrElement(4)*state.const.RTD, state.OrElement(1)*(1+state.OrElement(2))-6378, ... state.OrElement(1)*(1-state.OrElement(2))-6378, state.nx, state.nz); % 写入LamdaBWeiHeight文件 fprintf(state.fpCombined1, '%10.12f,%10.12f,%10.12f\n', state.Height, state.Lamda*state.const.RTD, state.BWei*state.const.RTD); end % 检查是否到达关机时间 if abs(state.TimeLeft - state.dh) < state.const.ErrorTime state.Flag_PowerOff = 1; end state.iflag = state.iflag + 1; end fprintf('滑翔第二次：%f %f %f %f %f %f\n', ... state.x0(1), state.Height, state.VEInorm, state.thetaK*state.const.RTD, state.alpha*state.const.RTD, state.phi*state.const.RTD); % ==================================================================== % 二级第二次开机 % ==================================================================== state.phase = 5; state.TimeLeft = state.const.TimeP22; state.Flag_PowerOff = 0; state.iflag = 0; while ~state.Flag_PowerOff if state.iflag ~= 0 state.TimeLeft = state.TimeLeft - state.dh; end if (state.TimeLeft < state.dh) && (abs(state.TimeLeft - state.dh) > state.const.ErrorTime) state.dh = state.TimeLeft; end % 执行龙格-库塔法积分 state.x0 = m_fnRK(state.x0, state.dh); % 调用动态计算函数获取所有参数 [state, dx] = m_fnDynamic(state); if state.Flag_write % 写入CombinedData文件 fprintf(state.fpCombined, '%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f,%10.12f\n', ... state.x0(1), state.x0(2), state.x0(3), state.x0(4), state.x0(5), state.x0(6), state.x0(7), ... state.phi*state.const.RTD, state.psi*state.const.RTD, state.gamma*state.const.RTD, ... state.theta*state.const.RTD, state.sigma*state.const.RTD, state.alpha*state.const.RTD, ... state.beta*state.const.RTD, state.Height, state.Vnorm, state.ma, state.MassRoc, ... state.thetaK*state.const.RTD, state.q, state.F_Engine(1), state.Lamda*state.const.RTD, ... state.BWei*state.const.RTD, state.Range, state.dW22(1), state.dW22(2), state.dW22(3), ... state.g(1), state.g(2), state.g(3), state.P*101.325, state.T, state.midu, ... state.OrElement(1), state.OrElement(2), state.OrElement(3)*state.const.RTD, ... state.OrElement(4)*state.const.RTD, state.OrElement(1)*(1+state.OrElement(2))-6378, ... state.OrElement(1)*(1-state.OrElement(2))-6378, state.nx, state.nz); % 写入LamdaBWeiHeight文件 fprintf(state.fpCombined1, '%10.12f,%10.12f,%10.12f\n', state.Height, state.Lamda*state.const.RTD, state.BWei*state.const.RTD); end % 检查是否到达关机时间 if abs(state.TimeLeft - state.dh) < state.const.ErrorTime state.Flag_PowerOff = 1; end state.iflag = state.iflag + 1; end fprintf('二级二次关机：%f %f %f %f %f %f\n', ... state.x0(1), state.Height, state.VEInorm, state.thetaK*state.const.RTD, state.alpha*state.const.RTD, state.phi*state.const.RTD); % 输出轨道参数 fprintf('半长轴：%f km\n', state.OrElement(1)); fprintf('偏心率：%f\n', state.OrElement(2)); fprintf('轨道倾角：%f °\n', state.OrElement(3)*state.const.RTD); fprintf('升交点赤经：%f °\n', state.OrElement(4)*state.const.RTD); fprintf('远地点高度：%f km\n', state.OrElement(1)*(1+state.OrElement(2))-6378); fprintf('近地点高度：%f km\n', state.OrElement(1)*(1-state.OrElement(2))-6378); % 关闭文件 if state.Flag_write && state.fpCombined ~= -1 fclose(state.fpCombined); end if state.Flag_write && state.fpCombined1 ~= -1 fclose(state.fpCombined1); end end
最新发布
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rad2deg([state.phi, state.psi, state.gamma, state.theta, state.sigma, state.alpha, state.beta]), ... state.Height, state.Vnorm, state.Ma, state.MassRoc, rad2deg(state.thetaK), ... state.q, state.F_...
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以上内容是根据“WakeUP_Poweroff.rar”压缩包中的资源，特别是“WakeUP_Poweroff”项目，对网络唤醒和Delphi编程实践的深入解析。对于希望学习网络唤醒技术，以及使用Delphi进行系统级编程的开发者来说，这些都是...
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qq_14877637的博客
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百里杨的博客
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1、概念理解 （1）扫盲 一个最简单的状态机应该包括状态机（QStateMachine）、状态(QState)和过渡（QAbstractTransition子类)。 状态机就相当于一个容器，过渡就是将某一个状态切换到另一个状态（当然也可以不切换）。 （2）什么时候可以用状态机 说的直白点就是，如果需要大量的if判断，然后判断的结果，下面又要判断走很多分支，但是这种分支状态是有限的，可...
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Eshare分享
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SimonLiu的博客
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hann的专栏
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前言： Vagrant是一个基于Ruby的工具，用于创建和部署虚拟化开发环境。 它的主要意义是让所有开发人员都使用和线上服务器一样的环境，本质上和你新建一个虚拟机。 那最常见的，正常我们是怎么开发呢，大部分童鞋应该是在windows下搭建开发环境，敲代码，运行程序，达到效果git或svn提交，发布linux环境再看效果。 而vagrant+virtualBox实现了把代码同步共...
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lzw5210的博客
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