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1 /* |
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2 * Copyright (c) 2005 Nokia Corporation and/or its subsidiary(-ies). |
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3 * All rights reserved. |
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4 * This component and the accompanying materials are made available |
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5 * under the terms of "Eclipse Public License v1.0" |
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6 * which accompanies this distribution, and is available |
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7 * at the URL "http://www.eclipse.org/legal/epl-v10.html". |
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8 * |
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9 * Initial Contributors: |
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10 * Nokia Corporation - initial contribution. |
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11 * |
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12 * Contributors: |
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13 * |
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14 * Description: This is a header file for engine class of Location satellite info |
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15 * |
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16 */ |
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17 |
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18 |
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19 #ifndef __SATELLITEENG_H__ |
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20 #define __SATELLITEENG_H__ |
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21 |
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22 // INCLUDES |
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23 #include <e32base.h> |
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24 #include <s32std.h> |
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25 #include <lbs.h> |
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26 #include <lbssatellite.h> |
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27 #include "MSatelliteEng.h" |
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28 #include "msatellitemeasurementsettingobserver.h" |
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29 |
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30 |
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31 // FORWARD DECLARATION |
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32 class CEikonEnv; |
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33 class CSatelliteMeasurementSetting; |
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34 // CLASS DECLARATION |
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35 /** |
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36 * |
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37 */ |
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38 NONSHARABLE_CLASS( CSatelliteEng ) : public CActive, public MSatelliteEng, |
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39 public MSatelliteMeasurementSettingObserver |
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40 { |
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41 public: |
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42 /** |
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43 * Two-phased constructor. |
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44 * |
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45 * @return CSatelliteEng object. |
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46 */ |
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47 static CSatelliteEng* NewL(); |
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48 |
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49 /** |
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50 * Destructor. |
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51 */ |
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52 ~CSatelliteEng(); |
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53 |
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54 private: |
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55 /** |
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56 * By default Symbian 2nd phase constructor is private. |
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57 */ |
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58 void ConstructL(); |
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59 |
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60 /** |
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61 * C++ default constructor. |
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62 */ |
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63 CSatelliteEng(); |
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64 |
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65 public: // from CActive |
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66 void RunL(); |
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67 void DoCancel(); |
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68 TInt RunError(TInt aError); |
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69 |
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70 private: //from MSatelliteEng |
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71 void SetObserver(MEngObserver& aObserver); |
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72 void RequestSatelliteDataL( const TDesC& aNameOfRule ); |
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73 TInt GetSatelliteData(TUint aIndex, |
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74 TSatelliteData& aSatelliteData) const; |
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75 |
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76 void GetPosition(TPosition& aPosition); |
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77 void GetCourse(TCourse& aCourse); |
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78 TLocSystemofMeasurementValues SysOfMeasurementL(); |
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79 TInt NumberOfSatellitesUsed(); |
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80 TInt NumberOfSatellites(); |
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81 void StopRequesting(); |
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82 void StartRequestingL(); |
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83 void SortVisibleSatellitesDataL(); |
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84 void UpdateIntervalL(); |
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85 void ClearSatelliteData(); |
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86 TBool IsSatelliteDataAvailable(); |
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87 void ObjectElevationAzimuth(TInt aIndex, TReal& aAzimuth, TReal& aElevation ); |
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88 void SortSatelliteDataL(); |
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89 void GetSunAzimuthElevation(TReal& aAzimuth, TReal& aElevation ); |
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90 void GetMoonAzimuthElevation(TReal& aAzimuth, TReal& aElevation ); |
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91 void Julian(TReal& aJulianDay, |
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92 TReal& aJulianCentury, |
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93 TInt aDay, |
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94 TInt aMonth, |
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95 TInt aYear, |
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96 TReal universalTime); |
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97 void TrueLongToRaDeltadec(TReal& aRa,TReal& aDd,TReal aTrueLongitude); |
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98 TReal Kepler(TReal aE, TReal aM); |
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99 void LocationCoordinates(TReal& aAzimuth, |
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100 TReal& aElevation, |
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101 TReal aTau, |
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102 TReal aDd, |
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103 TReal aLatitude); |
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104 TReal SideRealTime(TReal aJulianDay, |
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105 TReal aJulianCentury, |
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106 TReal aLongitude, |
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107 TReal aRa); |
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108 |
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109 private: //from MSatelliteMeasurementSettingObserver |
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110 void HandleSysMeasureValueL(); |
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111 |
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112 private: // data |
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113 /// Own: iServer |
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114 RPositionServer iServer; |
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115 |
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116 /// Own: RPositioner |
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117 RPositioner iPositioner; |
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118 |
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119 /// Own: TPositionSatelliteInfo |
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120 TPositionSatelliteInfo iSatelliteInfo; |
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121 |
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122 /// Own: CSatelliteMeasurementSetting |
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123 CSatelliteMeasurementSetting* iMeasurementSetting; |
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124 |
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125 /// Ref: Refrence to the observer for position notification |
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126 MEngObserver* iObserver; |
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127 |
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128 /// Own: Start and stop requesting |
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129 TBool iRequesting; |
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130 |
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131 /// Number of modules |
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132 TUint iNumberOfModules; |
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133 |
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134 /// used modules index |
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135 TInt iModuleIndex; |
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136 |
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137 /// used as an sorted index array to the satellite info data |
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138 TFixedArray<TUint8, KPositionMaxSatellitesInView> iSortIndices; |
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139 |
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140 // Own: Array to sort the satellite data in increasing order of |
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141 // the signal strengths |
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142 RArray<TSatelliteData> iSortedSatData; |
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143 |
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144 // Keplers constant for sun and moon position calculations |
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145 struct TKeplers |
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146 { |
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147 struct params |
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148 { |
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149 TReal iA0; |
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150 TReal iA1; |
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151 }; |
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152 params iM; |
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153 params iW; |
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154 params iE; |
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155 }; |
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156 TKeplers iKeplers[2]; |
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157 }; |
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158 |
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159 #endif // __SATELLITEENG_H__ |
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160 |
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161 // End of File |