1 | #LyX 1.6.4 created this file. For more info see http://www.lyx.org/ |
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2 | \lyxformat 345 |
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3 | \begin_document |
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4 | \begin_header |
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5 | \textclass scrartcl |
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6 | \begin_preamble |
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7 | \newcommand\blabl{} |
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8 | \end_preamble |
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9 | \use_default_options false |
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10 | \begin_modules |
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11 | theorems-ams |
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12 | theorems-ams-extended |
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13 | \end_modules |
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14 | \language english |
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15 | \inputencoding auto |
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16 | \font_roman lmodern |
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24 | |
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25 | \graphics default |
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26 | \paperfontsize default |
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27 | \spacing single |
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28 | \use_hyperref true |
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29 | \pdf_bookmarks true |
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40 | \use_amsmath 1 |
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41 | \use_esint 0 |
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42 | \cite_engine basic |
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43 | \use_bibtopic false |
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44 | \paperorientation portrait |
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45 | \secnumdepth 3 |
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46 | \tocdepth 3 |
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47 | \paragraph_separation indent |
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48 | \defskip medskip |
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49 | \quotes_language english |
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50 | \papercolumns 1 |
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51 | \papersides 1 |
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52 | \paperpagestyle default |
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53 | \tracking_changes false |
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54 | \output_changes false |
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55 | \author "" |
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56 | \author "" |
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57 | \end_header |
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58 | |
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59 | \begin_body |
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60 | |
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61 | \begin_layout Standard |
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62 | \begin_inset FormulaMacro |
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63 | \newcommand{\isa}[1]{i_{\alpha#1}} |
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64 | {i_{\alpha#1}} |
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65 | \end_inset |
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66 | |
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67 | |
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68 | \begin_inset FormulaMacro |
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69 | \newcommand{\isb}[1]{i_{\beta#1}} |
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70 | {i_{\beta#1}} |
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71 | \end_inset |
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72 | |
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73 | |
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74 | \begin_inset FormulaMacro |
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75 | \newcommand{\Dt}{\Delta t} |
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76 | {\Delta t} |
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77 | \end_inset |
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78 | |
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79 | |
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80 | \begin_inset FormulaMacro |
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81 | \newcommand{\om}{\omega} |
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82 | {\omega} |
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83 | \end_inset |
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84 | |
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85 | |
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86 | \begin_inset FormulaMacro |
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87 | \newcommand{\th}{\vartheta} |
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88 | {\vartheta} |
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89 | \end_inset |
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90 | |
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91 | |
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92 | \begin_inset FormulaMacro |
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93 | \newcommand{\usa}[1]{u_{\alpha#1}} |
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94 | {u_{\alpha#1}} |
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95 | \end_inset |
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96 | |
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97 | |
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98 | \begin_inset FormulaMacro |
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99 | \newcommand{\usb}[1]{u_{\beta#1}} |
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100 | {u_{\beta#1}} |
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101 | \end_inset |
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102 | |
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103 | |
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104 | \end_layout |
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105 | |
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106 | \begin_layout Title |
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107 | PMSM system description |
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108 | \end_layout |
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109 | |
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110 | \begin_layout Section |
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111 | Model of PMSM Drive |
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112 | \end_layout |
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113 | |
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114 | \begin_layout Standard |
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115 | Permanent magnet synchronous machine (PMSM) drive with surface magnets on |
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116 | the rotor is described by conventional equations of PMSM in the stationary |
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117 | reference frame: |
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118 | \begin_inset Formula \begin{align} |
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119 | \frac{d\isa{}}{dt} & =-\frac{R_{s}}{L_{s}}\isa{}+\frac{\Psi_{PM}}{L_{s}}\omega_{me}\sin\th+\frac{\usa{}}{L_{s}},\nonumber \\ |
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120 | \frac{d\isb{}}{dt} & =-\frac{R_{s}}{L_{s}}\isb{}-\frac{\Psi_{PM}}{L_{s}}\omega_{me}\cos\th+\frac{\usb{}}{L_{s}},\label{eq:simulator}\\ |
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121 | \frac{d\om}{dt} & =\frac{k_{p}p_{p}^{2}\Psi_{pm}}{J}\left(\isb{}\cos(\th)-\isa{}\sin(\th)\right)-\frac{B}{J}\om-\frac{p_{p}}{J}T_{L},\nonumber \\ |
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122 | \frac{d\th}{dt} & =\omega_{me}.\nonumber \end{align} |
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123 | |
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124 | \end_inset |
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125 | |
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126 | Here, |
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127 | \begin_inset Formula $\isa{}$ |
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128 | \end_inset |
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129 | |
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130 | , |
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131 | \begin_inset Formula $\isb{}$ |
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132 | \end_inset |
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133 | |
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134 | , |
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135 | \begin_inset Formula $\usa{}$ |
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136 | \end_inset |
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137 | |
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138 | and |
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139 | \begin_inset Formula $\usb{}$ |
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140 | \end_inset |
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141 | |
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142 | represent stator current and voltage in the stationary reference frame, |
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143 | respectively; |
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144 | \begin_inset Formula $\om$ |
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145 | \end_inset |
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146 | |
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147 | is electrical rotor speed and |
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148 | \begin_inset Formula $\th$ |
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149 | \end_inset |
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150 | |
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151 | is electrical rotor position. |
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152 | |
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153 | \begin_inset Formula $R_{s}$ |
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154 | \end_inset |
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155 | |
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156 | and |
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157 | \begin_inset Formula $L_{s}$ |
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158 | \end_inset |
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159 | |
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160 | is stator resistance and inductance respectively, |
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161 | \begin_inset Formula $\Psi_{pm}$ |
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162 | \end_inset |
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163 | |
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164 | is the flux of permanent magnets on the rotor, |
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165 | \begin_inset Formula $B$ |
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166 | \end_inset |
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167 | |
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168 | is friction and |
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169 | \begin_inset Formula $T_{L}$ |
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170 | \end_inset |
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171 | |
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172 | is load torque, |
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173 | \begin_inset Formula $J$ |
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174 | \end_inset |
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175 | |
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176 | is moment of inertia, |
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177 | \begin_inset Formula $p_{p}$ |
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178 | \end_inset |
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179 | |
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180 | is the number of pole pairs, |
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181 | \begin_inset Formula $k_{p}$ |
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182 | \end_inset |
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183 | |
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184 | is the Park constant. |
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185 | \end_layout |
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186 | |
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187 | \begin_layout Standard |
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188 | The sensor-less control scenario arise when sensors of the speed and position |
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189 | ( |
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190 | \begin_inset Formula $\om$ |
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191 | \end_inset |
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192 | |
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193 | and |
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194 | \begin_inset Formula $\th$ |
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195 | \end_inset |
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196 | |
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197 | ) are missing (from various reasons). |
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198 | Then, the only observed variables are: |
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199 | \begin_inset Formula \begin{equation} |
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200 | y_{t}=\left[\begin{array}{c} |
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201 | \isa{}(t),\isb{}(t),\usa{}(t),\usb{}(t)\end{array}\right].\label{eq:obs}\end{equation} |
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202 | |
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203 | \end_inset |
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204 | |
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205 | Which are, however, observed only up to some precision. |
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206 | \end_layout |
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207 | |
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208 | \begin_layout Standard |
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209 | Discretization of the model ( |
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210 | \begin_inset CommandInset ref |
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211 | LatexCommand ref |
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212 | reference "eq:simulator" |
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213 | |
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214 | \end_inset |
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215 | |
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216 | ) was performed using Euler method with the following result: |
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217 | \begin_inset Formula \begin{align*} |
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218 | \isa{,t+1} & =(1-\frac{R_{s}}{L_{s}}\Dt)\isa{,t}+\frac{\Psi_{pm}}{L_{s}}\Dt\omega_{t}\sin\vartheta_{e,t}+\usa{,t}\frac{\Dt}{L_{s}},\\ |
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219 | \isb{,t+1} & =(1-\frac{R_{s}}{L_{s}}\Dt)\isb{,t}-\frac{\Psi_{pm}}{L_{s}}\Dt\omega_{t}\cos\vartheta_{t}+\usb{,t}\frac{\Dt}{L_{s}},\\ |
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220 | \om_{t+1} & =(1--\frac{B}{J}\Dt)\om_{t}+\Dt\frac{k_{p}p_{p}^{2}\Psi_{pm}}{J}\left(\isb{,t}\cos(\th_{t})-\isa{,t}\sin(\th_{t})\right)-\frac{p_{p}}{J}T_{L}\Dt,\\ |
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221 | \vartheta_{t+1} & =\vartheta_{t}+\omega_{t}\Dt.\end{align*} |
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222 | |
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223 | \end_inset |
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224 | |
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225 | In this work, we consider parameters of the model known, we can make the |
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226 | following substitutions to simplify notation, |
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227 | \begin_inset Formula $a=1-\frac{R_{s}}{L_{s}}\Dt$ |
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228 | \end_inset |
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229 | |
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230 | , |
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231 | \begin_inset Formula $b=\frac{\Psi_{pm}}{L_{s}}\Dt$ |
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232 | \end_inset |
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233 | |
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234 | , |
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235 | \begin_inset Formula $c=\frac{\Dt}{L_{s}}$ |
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236 | \end_inset |
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237 | |
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238 | , |
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239 | \begin_inset Formula $d=1-\frac{B}{J}\Dt$ |
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240 | \end_inset |
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241 | |
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242 | , |
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243 | \family roman |
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244 | \series medium |
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245 | \shape up |
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246 | \size normal |
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247 | \emph off |
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248 | \bar no |
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249 | \noun off |
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250 | \color none |
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251 | |
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252 | \begin_inset Formula $e=\Dt\frac{k_{p}p_{p}^{2}\Psi_{pm}}{J}$ |
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253 | \end_inset |
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254 | |
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255 | , which results in a simplified model: |
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256 | \family default |
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257 | \series default |
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258 | \shape default |
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259 | \size default |
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260 | \emph default |
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261 | \bar default |
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262 | \noun default |
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263 | \color inherit |
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264 | |
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265 | \begin_inset Formula \begin{align} |
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266 | \isa{,t+1} & =a\,\isa{,t}+b\omega_{t}\sin\vartheta_{t}+c\usa{,t},\nonumber \\ |
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267 | \isb{,t+1} & =a\,\isb{,t}-b\omega_{t}\cos\vartheta_{t}+c\usb{,t},\label{eq:model-simple}\\ |
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268 | \om_{t+1} & =d\om_{t}+e\left(\isb{,t}\cos(\th_{t})-\isa{,t}\sin(\th_{t})\right),\nonumber \\ |
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269 | \vartheta_{t+1} & =\vartheta_{t}+\omega_{t}\Dt.\nonumber \end{align} |
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270 | |
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271 | \end_inset |
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272 | |
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273 | |
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274 | \end_layout |
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275 | |
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276 | \begin_layout Standard |
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277 | The above equations can be aggregated into state |
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278 | \begin_inset Formula $x_{t}=[\isa{,t},\isb{,t},\om_{t},\th_{t}]$ |
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279 | \end_inset |
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280 | |
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281 | will be denoted as |
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282 | \begin_inset Formula $x_{t+1}=g(x_{t},u_{t})$ |
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283 | \end_inset |
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284 | |
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285 | . |
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286 | \end_layout |
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287 | |
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288 | \begin_layout Subsection |
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289 | Gaussian model of disturbances |
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290 | \end_layout |
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291 | |
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292 | \begin_layout Standard |
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293 | This model is motivated by the well known Kalman filter, which is optimal |
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294 | for linear system with Gaussian noise. |
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295 | Hence, we model all disturbances to have covariance matrices |
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296 | \begin_inset Formula $Q_{t}$ |
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297 | \end_inset |
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298 | |
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299 | and |
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300 | \begin_inset Formula $R_{t}$ |
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301 | \end_inset |
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302 | |
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303 | for the state |
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304 | \begin_inset Formula $x_{t}$ |
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305 | \end_inset |
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306 | |
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307 | and observations |
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308 | \begin_inset Formula $y_{t}$ |
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309 | \end_inset |
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310 | |
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311 | respectively. |
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312 | \begin_inset Formula \begin{align*} |
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313 | x_{t+1} & \sim\mathcal{N}(g(x_{t}),Q_{t})\\ |
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314 | y_{t} & \sim\mathcal{N}([\isa{,t},\isb{,t}]',R_{t})\end{align*} |
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315 | |
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316 | \end_inset |
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317 | |
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318 | |
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319 | \end_layout |
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320 | |
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321 | \begin_layout Standard |
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322 | Under this assumptions, Bayesian estimation of the state, |
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323 | \begin_inset Formula $x_{t}$ |
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324 | \end_inset |
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325 | |
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326 | , can be approximated by so called Extended Kalman filter which approximates |
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327 | posterior density of the state by a Gaussian |
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328 | \begin_inset Formula \[ |
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329 | f(x_{t}|y_{1}\ldots y_{t})=\mathcal{N}(\hat{x}_{t},P_{t}).\] |
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330 | |
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331 | \end_inset |
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332 | |
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333 | Its sufficient statistics |
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334 | \begin_inset Formula $S_{t}=\left[\hat{x}_{t},P_{t}\right]$ |
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335 | \end_inset |
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336 | |
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337 | is evaluated recursively as follows: |
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338 | \begin_inset Formula \begin{eqnarray} |
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339 | \hat{x}_{t} & = & g(\hat{x}_{t-1})-K\left(y_{t}-h(\hat{x}_{t-1})\right).\label{eq:ekf_mean}\\ |
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340 | R_{y} & = & C'P_{t-1}C+R_{t},\nonumber \\ |
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341 | K & = & P_{t-1}CR_{y}^{-1}(y_{t}-h(\hat{x}_{t-1})),\nonumber \\ |
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342 | P_{t} & = & A\left(P_{t-1}-P_{t-1}C'R_{y}^{-1}CP_{t-1}\right)A+Q_{t}.\label{eq:ekf_cov}\end{eqnarray} |
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343 | |
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344 | \end_inset |
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345 | |
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346 | where |
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347 | \begin_inset Formula $A=\frac{d}{dx_{t}}g(x_{t})$ |
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348 | \end_inset |
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349 | |
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350 | , |
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351 | \begin_inset Formula $C=\frac{d}{dx_{t}}h(x_{t})$ |
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352 | \end_inset |
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353 | |
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354 | , |
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355 | \begin_inset Formula $g(x_{t})$ |
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356 | \end_inset |
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357 | |
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358 | is model ( |
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359 | \begin_inset CommandInset ref |
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360 | LatexCommand ref |
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361 | reference "eq:model-simple" |
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362 | |
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363 | \end_inset |
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364 | |
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365 | ) and |
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366 | \begin_inset Formula $h(x_{t})$ |
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367 | \end_inset |
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368 | |
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369 | direct observation of |
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370 | \begin_inset Formula $y_{t}=[\isa{,t},\isb{,t}]$ |
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371 | \end_inset |
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372 | |
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373 | , i.e. |
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374 | \begin_inset Formula \[ |
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375 | A=\left[\begin{array}{cccc} |
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376 | a & 0 & b\sin\th & b\om\cos\th\\ |
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377 | 0 & a & -b\cos\th & b\om\sin\th\\ |
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378 | -e\sin\th & e\cos\th & d & -e(\isb{}\sin\th+\isa{}\cos\th)\\ |
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379 | 0 & 0 & \Dt & 1\end{array}\right],\quad C=\left[\begin{array}{cccc} |
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380 | 1\\ |
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381 | & 1\\ |
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382 | & & 0\\ |
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383 | & & & 0\end{array}\right]\] |
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384 | |
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385 | \end_inset |
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386 | |
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387 | |
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388 | \end_layout |
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389 | |
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390 | \begin_layout Standard |
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391 | Covariance matrices of the system |
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392 | \begin_inset Formula $Q$ |
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393 | \end_inset |
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394 | |
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395 | and |
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396 | \begin_inset Formula $R$ |
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397 | \end_inset |
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398 | |
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399 | are supposed to be known. |
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400 | \end_layout |
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401 | |
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402 | \begin_layout Section |
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403 | Control |
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404 | \end_layout |
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405 | |
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406 | \begin_layout Standard |
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407 | The task is to reach predefined speed |
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408 | \begin_inset Formula $\overline{\omega}_{t}$ |
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409 | \end_inset |
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410 | |
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411 | . |
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412 | \end_layout |
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413 | |
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414 | \begin_layout Standard |
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415 | For simplicity, we will assume additive loss function: |
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416 | \begin_inset Formula \[ |
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417 | l(x_{t},u_{t})=(\omega_{t}-\overline{\omega}_{t})^{2}+\psi(\usa{,t}^{2}+\usb{,t}^{2}).\] |
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418 | |
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419 | \end_inset |
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420 | |
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421 | Here, |
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422 | \begin_inset Formula $\psi$ |
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423 | \end_inset |
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424 | |
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425 | is the chosen penalization of the inputs. |
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426 | |
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427 | \end_layout |
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428 | |
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429 | \begin_layout Standard |
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430 | Following the standard dynamic programming approach, optimization of the |
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431 | loss function can be done recursively, as follows: |
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432 | \begin_inset Formula \[ |
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433 | V(x_{t-1},u_{t-1})=\arg\min_{u_{t}}\mathsf{E}_{f(x_{t},y_{t}|x_{t-1})}\left\{ l(x_{t},u_{t})+V(x_{t},u_{t})\right\} ,\] |
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434 | |
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435 | \end_inset |
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436 | |
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437 | where |
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438 | \begin_inset Formula $V(x_{t},u_{t})$ |
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439 | \end_inset |
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440 | |
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441 | is the Bellman function. |
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442 | Since the model evolution is stochastic, we can reformulate it in terms |
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443 | of sufficient statistics, |
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444 | \begin_inset Formula $S$ |
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445 | \end_inset |
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446 | |
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447 | as follows: |
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448 | \begin_inset Formula \[ |
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449 | V(S_{t-1})=\min_{u_{t}}\mathsf{E}_{f(x_{t},y_{t}|x_{t-1})}\left\{ l(x_{t},u_{t})+V(S_{t})\right\} .\] |
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450 | |
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451 | \end_inset |
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452 | |
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453 | |
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454 | \end_layout |
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455 | |
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456 | \begin_layout Standard |
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457 | Representation of the Bellman function depends on chosen approximation. |
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458 | \end_layout |
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459 | |
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460 | \begin_layout Standard |
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461 | \begin_inset CommandInset bibtex |
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462 | LatexCommand bibtex |
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463 | bibfiles "bibtex/vs,bibtex/vs-world,bibtex/world_classics,bibtex/world,new_bib_PS" |
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464 | options "plain" |
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465 | |
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466 | \end_inset |
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467 | |
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468 | |
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469 | \end_layout |
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470 | |
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471 | \end_body |
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472 | \end_document |
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