1 | function OCS = setorbitV(varargin) |
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2 | %SETORBITV - Correct the horizontal orbit |
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3 | % |
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4 | % INPUTS |
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5 | % 1. GoalOrbit - Goal orbit (vector or cell array (if BPM is a cell array)) |
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6 | % 'Golden' for the golden orbit {Default} |
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7 | % 'Offset' for the offset orbit |
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8 | % 2. BPM - BPMDevList |
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9 | % 3. CM - CMDevList |
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10 | % 4. SVDIndex - vector, maximum number, 'All', or |
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11 | % base on a threshold of min/max singular value {Default: 1e-3} |
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12 | % 5. NIter - Number of iterations {Default: 1} |
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13 | % (NIter can be 0, see note 1 below) |
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14 | % 6. BPMWeight - Weight applied to the BPMs (OCS.BPMWeight) |
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15 | % 7. FLAGS - 'Abs' or 'Absolute' - GoalOrbit is an absolute orbit {Default} |
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16 | % 'Inc' or 'Incremental' - GoalOrbit is a incremental change |
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17 | % 'ModelResp' - calculate the model response matrix {Default: measured response matrix} |
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18 | % 'SetSP' - Make the setpoint change {Default} |
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19 | % 'NoSetSP' - Don't set the magnets, just return the OCS |
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20 | % 'Display' - plot orbit information before applying the correction |
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21 | % 'FitRF' - Fit and change the RF frequency (use rmdisp before |
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22 | % calling this function to remove the dispersion orbit) |
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23 | % 'MeasDisp' - measure the dispersion {Default} |
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24 | % 'ModelDisp' - calculate the model dispersion |
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25 | % 'GoldenDisp' - use the golden dispersion |
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26 | % And the usual Units and Mode flags |
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27 | % |
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28 | % OUTPUTS |
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29 | % 1. OCS - New orbit correction structure (OCS) |
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30 | % |
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31 | % See Also setorbit, setorbitV |
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32 | |
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33 | % |
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34 | %% Written by Laurent S. Nadolski |
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35 | |
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36 | TypeFlag = 'SOFB'; |
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37 | GoldenFlag = 0; |
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38 | % Default BPM Family |
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39 | BPMFamily = getvbpmfamily; |
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40 | BPMlist = []; |
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41 | |
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42 | % Default corrector Family |
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43 | CMlist = []; |
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44 | |
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45 | OCSFlags = []; |
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46 | InputFlags = []; |
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47 | |
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48 | % Defaults values |
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49 | OCS.NIter = 1; % Number of iteration |
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50 | OCS.SVDIndex = 56; % number of eigenvector for correction |
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51 | OCS.IncrementalFlag = 'No'; |
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52 | OCS.FitRF = 0; % take RF as a corrector |
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53 | |
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54 | % Input parsing |
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55 | for i = length(varargin):-1:1 |
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56 | if isstruct(varargin{i}) |
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57 | % Ignore structures |
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58 | elseif iscell(varargin{i}) |
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59 | % Ignore cells |
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60 | elseif strcmpi(varargin{i},'Golden') |
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61 | % Use the golden orbit |
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62 | OCS.GoalOrbit = 'Golden'; |
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63 | OCSFlags = [OCSFlags varargin(i)]; |
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64 | varargin(i) = []; |
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65 | elseif strcmpi(varargin{i},'Offset') |
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66 | % Use the offset orbit |
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67 | OCS.GoalOrbit = 'Offset'; |
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68 | OCSFlags = [OCSFlags varargin(i)]; |
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69 | varargin(i) = []; |
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70 | elseif strcmpi(varargin{i},'Display') |
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71 | OCSFlags = [OCSFlags varargin(i)]; |
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72 | varargin(i) = []; |
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73 | elseif strcmpi(varargin{i},'NoDisplay') || ... |
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74 | strcmpi(varargin{i},'No Display') |
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75 | InputFlags = [InputFlags varargin(i)]; |
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76 | varargin(i) = []; |
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77 | elseif strcmpi(varargin{i},'ModelResp') |
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78 | OCSFlags = [OCSFlags varargin(i)]; |
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79 | varargin(i) = []; |
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80 | elseif strcmpi(varargin{i},'FitRF') |
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81 | OCSFlags = [OCSFlags varargin(i)]; |
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82 | varargin(i) = []; |
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83 | elseif strcmpi(varargin{i},'ModelDisp') |
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84 | OCSFlags = [OCSFlags varargin(i)]; |
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85 | varargin(i) = []; |
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86 | elseif strcmpi(varargin{i},'MeasDisp') |
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87 | OCSFlags = [OCSFlags varargin(i)]; |
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88 | varargin(i) = []; |
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89 | elseif strcmpi(varargin{i},'GoldenDisp') |
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90 | OCSFlags = [OCSFlags varargin(i)]; |
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91 | varargin(i) = []; |
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92 | elseif strcmpi(varargin{i},'Inc') || strcmpi(varargin{i},'Incremental') |
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93 | OCSFlags = [OCSFlags varargin(i)]; |
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94 | varargin(i) = []; |
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95 | elseif strcmpi(varargin{i},'Abs') || strcmpi(varargin{i},'Absolute') |
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96 | OCSFlags = [OCSFlags varargin(i)]; |
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97 | elseif strcmpi(varargin{i},'SetSP') |
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98 | InputFlags = [InputFlags varargin(i)]; |
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99 | varargin(i) = []; |
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100 | elseif strcmpi(varargin{i},'NoSetSP') |
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101 | InputFlags = [InputFlags varargin(i)]; |
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102 | varargin(i) = []; |
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103 | elseif strcmpi(varargin{i},'Simulator') || strcmpi(varargin{i},'Model') |
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104 | OCSFlags = [OCSFlags varargin(i)]; |
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105 | InputFlags = [InputFlags varargin(i)]; |
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106 | varargin(i) = []; |
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107 | elseif strcmpi(varargin{i},'Online') |
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108 | OCSFlags = [OCSFlags varargin(i)]; |
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109 | InputFlags = [InputFlags varargin(i)]; |
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110 | varargin(i) = []; |
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111 | elseif strcmpi(varargin{i},'Manual') |
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112 | OCSFlags = [OCSFlags varargin(i)]; |
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113 | InputFlags = [InputFlags varargin(i)]; |
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114 | varargin(i) = []; |
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115 | elseif strcmpi(varargin{i},'Physics') |
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116 | OCSFlags = [OCSFlags varargin(i)]; |
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117 | InputFlags = [InputFlags varargin(i)]; |
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118 | varargin(i) = []; |
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119 | elseif strcmpi(varargin{i},'Hardware') |
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120 | OCSFlags = [OCSFlags varargin(i)]; |
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121 | InputFlags = [InputFlags varargin(i)]; |
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122 | varargin(i) = []; |
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123 | elseif strcmpi(varargin{i},'Archive') |
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124 | % Just remove |
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125 | varargin(i) = []; |
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126 | elseif strcmpi(varargin{i},'noarchive') |
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127 | % Just remove |
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128 | varargin(i) = []; |
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129 | elseif strcmpi(varargin{i},'struct') |
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130 | % Just remove |
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131 | varargin(i) = []; |
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132 | elseif strcmpi(varargin{i},'numeric') |
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133 | % Just remove |
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134 | varargin(i) = []; |
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135 | elseif strcmpi(varargin{i},'FOFB') |
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136 | TypeFlag = 'FOFB'; |
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137 | varargin(i) = []; |
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138 | elseif strcmpi(varargin{i},'SOFB') |
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139 | TypeFlag = 'SOFB'; |
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140 | varargin(i) = []; |
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141 | end |
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142 | end |
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143 | |
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144 | % switchard for typical orbit correction at SOLEIL |
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145 | switch TypeFlag |
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146 | case 'FOFB' |
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147 | % number of eigenvector for correction |
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148 | OCS.SVDIndex = 40; |
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149 | % Default corrector Family |
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150 | CMFamily = 'FVCOR'; |
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151 | case 'SOFB' |
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152 | % number of eigenvector for correction |
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153 | OCS.SVDIndex = 56; |
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154 | % Default corrector Family |
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155 | CMFamily = 'VCOR'; |
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156 | otherwise |
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157 | error('TypeFlag invalid') |
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158 | end |
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159 | % Get Goal orbit |
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160 | if length(varargin) >= 1 |
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161 | OCS.GoalOrbit = varargin{1}; |
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162 | varargin(1) = []; |
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163 | end |
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164 | |
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165 | % Get BPM knobs |
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166 | if length(varargin) >= 1 |
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167 | BPMlist = varargin{1}; |
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168 | varargin(1) = []; |
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169 | end |
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170 | |
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171 | % Get CM knobs |
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172 | if length(varargin) >= 1 |
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173 | CMlist = varargin{1}; |
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174 | varargin(1) = []; |
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175 | end |
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176 | |
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177 | % Get SVDIndex |
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178 | if length(varargin) >= 1 |
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179 | OCS.SVDIndex = varargin{1}; |
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180 | varargin(1) = []; |
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181 | end |
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182 | |
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183 | % Get NIter |
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184 | if length(varargin) >= 1 |
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185 | OCS.NIter = varargin{1}; |
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186 | varargin(1) = []; |
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187 | end |
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188 | |
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189 | % Get BPMWeight |
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190 | if length(varargin) >= 1 |
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191 | OCS.BPMWeight = varargin{1}; |
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192 | varargin(1) = []; |
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193 | end |
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194 | |
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195 | Zgoal = getgolden(BPMFamily, BPMlist); |
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196 | |
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197 | %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% |
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198 | % Build up Orbit correction Structures % |
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199 | % for setorbit programme : OCSx and OCSy% |
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200 | %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% |
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201 | % ORBIT CORRECTION STRUCTURE (OCS) |
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202 | % OCS.BPM (data structure) |
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203 | % OCS.CM (data structure) |
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204 | % OCS.GoalOrbit |
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205 | % OCS.NIter |
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206 | % OCS.SVDIndex |
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207 | % OCS.IncrementalFlag = 'Yes'/'No' |
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208 | % OCS.BPMWeight |
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209 | % OCS.Flags = { 'FitRF' , etc. } |
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210 | |
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211 | % Horizontal plane |
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212 | OCS.BPM = getz(BPMlist, 'struct'); |
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213 | OCS.GoalOrbit = Zgoal; |
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214 | OCS.CM = getsp(CMFamily, CMlist, 'struct'); |
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215 | OCS.Flags = OCSFlags; |
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216 | |
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217 | if isempty(InputFlags) |
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218 | OCS = setorbit(OCS); |
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219 | else |
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220 | OCS = setorbit(OCS,InputFlags{:}); |
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221 | end |
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