Mathematical model of the sensor unit for processing on-board algorithms of navigation systems

Abstract Recently, strapdown gyro navigation systems have become widely used. In such systems, sensors, gyros, and accelerometers are placed directly aboard the object and an imaginary analytic trihedral is used instead of a stabilized gyroplatform. The object orientation with respect to the analyti...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Alekhova, E. Yu. [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2008

Schlagwörter:	Navigation System Inertial Navigation System Sensor Unit Platform System Navigation Problem

Übergeordnetes Werk:	Enthalten in: Mechanics of solids - New York, NY : Allerton, 2007, 43(2008), 3 vom: Juni, Seite 349-353
Übergeordnetes Werk:	volume:43 ; year:2008 ; number:3 ; month:06 ; pages:349-353

Links:	Volltext

DOI / URN:	10.3103/S0025654408030060

Katalog-ID:	SPR023254521

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520			\|a Abstract Recently, strapdown gyro navigation systems have become widely used. In such systems, sensors, gyros, and accelerometers are placed directly aboard the object and an imaginary analytic trihedral is used instead of a stabilized gyroplatform. The object orientation with respect to the analytic trihedral is calculated by numerically solving the Poisson equations taking into account the readings of gyro sensors measuring the object angular velocities. The mutual orientation parameters permit recalculating the apparent acceleration measured by the accelerometers on the object axes for the axes of the analytic trihedral. In the analytic trihedral, the navigation problem is solved in the same way as it is solved in platform systems but, in the whole, the functions of the onboard algorithms of strapdown systems are significantly more complicated than those of platform systems. The possibility of detailed processing of on-board algorithms is of great importance for ensuring the accuracy of the entire navigation system. In the present paper, we state algorithms for reproducing the exact readings of ideal gyro sensors and the exact readings of ideal accelerometers under bench operating conditions of the system under an angular motion imitating the object orientation evolution and the possible angular vibration. Simultaneously, we calculate the exact position and orientation parameters, which can be compared with the results produced by the on-board algorithm.
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650		4	\|a Navigation Problem \|7 (dpeaa)DE-He213
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912			\|a GBV_ILN_151
912			\|a GBV_ILN_152
912			\|a GBV_ILN_161
912			\|a GBV_ILN_170
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912			\|a GBV_ILN_602
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912			\|a GBV_ILN_2010
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912			\|a GBV_ILN_2025
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matchkey_str	article:19347936:2008----::ahmtcloeoteesrntopoesnobadloih
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publishDate	2008
allfields	10.3103/S0025654408030060 doi (DE-627)SPR023254521 (SPR)S0025654408030060-e DE-627 ger DE-627 rakwb eng 600 ASE Alekhova, E. Yu. verfasserin aut Mathematical model of the sensor unit for processing on-board algorithms of navigation systems 2008 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract Recently, strapdown gyro navigation systems have become widely used. In such systems, sensors, gyros, and accelerometers are placed directly aboard the object and an imaginary analytic trihedral is used instead of a stabilized gyroplatform. The object orientation with respect to the analytic trihedral is calculated by numerically solving the Poisson equations taking into account the readings of gyro sensors measuring the object angular velocities. The mutual orientation parameters permit recalculating the apparent acceleration measured by the accelerometers on the object axes for the axes of the analytic trihedral. In the analytic trihedral, the navigation problem is solved in the same way as it is solved in platform systems but, in the whole, the functions of the onboard algorithms of strapdown systems are significantly more complicated than those of platform systems. The possibility of detailed processing of on-board algorithms is of great importance for ensuring the accuracy of the entire navigation system. In the present paper, we state algorithms for reproducing the exact readings of ideal gyro sensors and the exact readings of ideal accelerometers under bench operating conditions of the system under an angular motion imitating the object orientation evolution and the possible angular vibration. Simultaneously, we calculate the exact position and orientation parameters, which can be compared with the results produced by the on-board algorithm. Navigation System (dpeaa)DE-He213 Inertial Navigation System (dpeaa)DE-He213 Sensor Unit (dpeaa)DE-He213 Platform System (dpeaa)DE-He213 Navigation Problem (dpeaa)DE-He213 Enthalten in Mechanics of solids New York, NY : Allerton, 2007 43(2008), 3 vom: Juni, Seite 349-353 (DE-627)535186789 (DE-600)2375720-6 1934-7936 nnns volume:43 year:2008 number:3 month:06 pages:349-353 https://dx.doi.org/10.3103/S0025654408030060 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 43 2008 3 06 349-353
spelling	10.3103/S0025654408030060 doi (DE-627)SPR023254521 (SPR)S0025654408030060-e DE-627 ger DE-627 rakwb eng 600 ASE Alekhova, E. Yu. verfasserin aut Mathematical model of the sensor unit for processing on-board algorithms of navigation systems 2008 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract Recently, strapdown gyro navigation systems have become widely used. In such systems, sensors, gyros, and accelerometers are placed directly aboard the object and an imaginary analytic trihedral is used instead of a stabilized gyroplatform. The object orientation with respect to the analytic trihedral is calculated by numerically solving the Poisson equations taking into account the readings of gyro sensors measuring the object angular velocities. The mutual orientation parameters permit recalculating the apparent acceleration measured by the accelerometers on the object axes for the axes of the analytic trihedral. In the analytic trihedral, the navigation problem is solved in the same way as it is solved in platform systems but, in the whole, the functions of the onboard algorithms of strapdown systems are significantly more complicated than those of platform systems. The possibility of detailed processing of on-board algorithms is of great importance for ensuring the accuracy of the entire navigation system. In the present paper, we state algorithms for reproducing the exact readings of ideal gyro sensors and the exact readings of ideal accelerometers under bench operating conditions of the system under an angular motion imitating the object orientation evolution and the possible angular vibration. Simultaneously, we calculate the exact position and orientation parameters, which can be compared with the results produced by the on-board algorithm. Navigation System (dpeaa)DE-He213 Inertial Navigation System (dpeaa)DE-He213 Sensor Unit (dpeaa)DE-He213 Platform System (dpeaa)DE-He213 Navigation Problem (dpeaa)DE-He213 Enthalten in Mechanics of solids New York, NY : Allerton, 2007 43(2008), 3 vom: Juni, Seite 349-353 (DE-627)535186789 (DE-600)2375720-6 1934-7936 nnns volume:43 year:2008 number:3 month:06 pages:349-353 https://dx.doi.org/10.3103/S0025654408030060 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 43 2008 3 06 349-353
allfields_unstemmed	10.3103/S0025654408030060 doi (DE-627)SPR023254521 (SPR)S0025654408030060-e DE-627 ger DE-627 rakwb eng 600 ASE Alekhova, E. Yu. verfasserin aut Mathematical model of the sensor unit for processing on-board algorithms of navigation systems 2008 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract Recently, strapdown gyro navigation systems have become widely used. In such systems, sensors, gyros, and accelerometers are placed directly aboard the object and an imaginary analytic trihedral is used instead of a stabilized gyroplatform. The object orientation with respect to the analytic trihedral is calculated by numerically solving the Poisson equations taking into account the readings of gyro sensors measuring the object angular velocities. The mutual orientation parameters permit recalculating the apparent acceleration measured by the accelerometers on the object axes for the axes of the analytic trihedral. In the analytic trihedral, the navigation problem is solved in the same way as it is solved in platform systems but, in the whole, the functions of the onboard algorithms of strapdown systems are significantly more complicated than those of platform systems. The possibility of detailed processing of on-board algorithms is of great importance for ensuring the accuracy of the entire navigation system. In the present paper, we state algorithms for reproducing the exact readings of ideal gyro sensors and the exact readings of ideal accelerometers under bench operating conditions of the system under an angular motion imitating the object orientation evolution and the possible angular vibration. Simultaneously, we calculate the exact position and orientation parameters, which can be compared with the results produced by the on-board algorithm. Navigation System (dpeaa)DE-He213 Inertial Navigation System (dpeaa)DE-He213 Sensor Unit (dpeaa)DE-He213 Platform System (dpeaa)DE-He213 Navigation Problem (dpeaa)DE-He213 Enthalten in Mechanics of solids New York, NY : Allerton, 2007 43(2008), 3 vom: Juni, Seite 349-353 (DE-627)535186789 (DE-600)2375720-6 1934-7936 nnns volume:43 year:2008 number:3 month:06 pages:349-353 https://dx.doi.org/10.3103/S0025654408030060 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 43 2008 3 06 349-353
allfieldsGer	10.3103/S0025654408030060 doi (DE-627)SPR023254521 (SPR)S0025654408030060-e DE-627 ger DE-627 rakwb eng 600 ASE Alekhova, E. Yu. verfasserin aut Mathematical model of the sensor unit for processing on-board algorithms of navigation systems 2008 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract Recently, strapdown gyro navigation systems have become widely used. In such systems, sensors, gyros, and accelerometers are placed directly aboard the object and an imaginary analytic trihedral is used instead of a stabilized gyroplatform. The object orientation with respect to the analytic trihedral is calculated by numerically solving the Poisson equations taking into account the readings of gyro sensors measuring the object angular velocities. The mutual orientation parameters permit recalculating the apparent acceleration measured by the accelerometers on the object axes for the axes of the analytic trihedral. In the analytic trihedral, the navigation problem is solved in the same way as it is solved in platform systems but, in the whole, the functions of the onboard algorithms of strapdown systems are significantly more complicated than those of platform systems. The possibility of detailed processing of on-board algorithms is of great importance for ensuring the accuracy of the entire navigation system. In the present paper, we state algorithms for reproducing the exact readings of ideal gyro sensors and the exact readings of ideal accelerometers under bench operating conditions of the system under an angular motion imitating the object orientation evolution and the possible angular vibration. Simultaneously, we calculate the exact position and orientation parameters, which can be compared with the results produced by the on-board algorithm. Navigation System (dpeaa)DE-He213 Inertial Navigation System (dpeaa)DE-He213 Sensor Unit (dpeaa)DE-He213 Platform System (dpeaa)DE-He213 Navigation Problem (dpeaa)DE-He213 Enthalten in Mechanics of solids New York, NY : Allerton, 2007 43(2008), 3 vom: Juni, Seite 349-353 (DE-627)535186789 (DE-600)2375720-6 1934-7936 nnns volume:43 year:2008 number:3 month:06 pages:349-353 https://dx.doi.org/10.3103/S0025654408030060 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 43 2008 3 06 349-353
allfieldsSound	10.3103/S0025654408030060 doi (DE-627)SPR023254521 (SPR)S0025654408030060-e DE-627 ger DE-627 rakwb eng 600 ASE Alekhova, E. Yu. verfasserin aut Mathematical model of the sensor unit for processing on-board algorithms of navigation systems 2008 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract Recently, strapdown gyro navigation systems have become widely used. In such systems, sensors, gyros, and accelerometers are placed directly aboard the object and an imaginary analytic trihedral is used instead of a stabilized gyroplatform. The object orientation with respect to the analytic trihedral is calculated by numerically solving the Poisson equations taking into account the readings of gyro sensors measuring the object angular velocities. The mutual orientation parameters permit recalculating the apparent acceleration measured by the accelerometers on the object axes for the axes of the analytic trihedral. In the analytic trihedral, the navigation problem is solved in the same way as it is solved in platform systems but, in the whole, the functions of the onboard algorithms of strapdown systems are significantly more complicated than those of platform systems. The possibility of detailed processing of on-board algorithms is of great importance for ensuring the accuracy of the entire navigation system. In the present paper, we state algorithms for reproducing the exact readings of ideal gyro sensors and the exact readings of ideal accelerometers under bench operating conditions of the system under an angular motion imitating the object orientation evolution and the possible angular vibration. Simultaneously, we calculate the exact position and orientation parameters, which can be compared with the results produced by the on-board algorithm. Navigation System (dpeaa)DE-He213 Inertial Navigation System (dpeaa)DE-He213 Sensor Unit (dpeaa)DE-He213 Platform System (dpeaa)DE-He213 Navigation Problem (dpeaa)DE-He213 Enthalten in Mechanics of solids New York, NY : Allerton, 2007 43(2008), 3 vom: Juni, Seite 349-353 (DE-627)535186789 (DE-600)2375720-6 1934-7936 nnns volume:43 year:2008 number:3 month:06 pages:349-353 https://dx.doi.org/10.3103/S0025654408030060 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 43 2008 3 06 349-353
language	English
source	Enthalten in Mechanics of solids 43(2008), 3 vom: Juni, Seite 349-353 volume:43 year:2008 number:3 month:06 pages:349-353
sourceStr	Enthalten in Mechanics of solids 43(2008), 3 vom: Juni, Seite 349-353 volume:43 year:2008 number:3 month:06 pages:349-353
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	Navigation System Inertial Navigation System Sensor Unit Platform System Navigation Problem
dewey-raw	600
isfreeaccess_bool	false
container_title	Mechanics of solids
authorswithroles_txt_mv	Alekhova, E. Yu. @@aut@@
publishDateDaySort_date	2008-06-01T00:00:00Z
hierarchy_top_id	535186789
dewey-sort	3600
id	SPR023254521
language_de	englisch
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author	Alekhova, E. Yu.
spellingShingle	Alekhova, E. Yu. ddc 600 misc Navigation System misc Inertial Navigation System misc Sensor Unit misc Platform System misc Navigation Problem Mathematical model of the sensor unit for processing on-board algorithms of navigation systems
authorStr	Alekhova, E. Yu.
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issn	1934-7936
topic_title	600 ASE Mathematical model of the sensor unit for processing on-board algorithms of navigation systems Navigation System (dpeaa)DE-He213 Inertial Navigation System (dpeaa)DE-He213 Sensor Unit (dpeaa)DE-He213 Platform System (dpeaa)DE-He213 Navigation Problem (dpeaa)DE-He213
topic	ddc 600 misc Navigation System misc Inertial Navigation System misc Sensor Unit misc Platform System misc Navigation Problem
topic_unstemmed	ddc 600 misc Navigation System misc Inertial Navigation System misc Sensor Unit misc Platform System misc Navigation Problem
topic_browse	ddc 600 misc Navigation System misc Inertial Navigation System misc Sensor Unit misc Platform System misc Navigation Problem
format_facet	Elektronische Aufsätze Aufsätze Elektronische Ressource
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hierarchy_parent_title	Mechanics of solids
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title	Mathematical model of the sensor unit for processing on-board algorithms of navigation systems
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title_full	Mathematical model of the sensor unit for processing on-board algorithms of navigation systems
author_sort	Alekhova, E. Yu.
journal	Mechanics of solids
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author_browse	Alekhova, E. Yu.
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class	600 ASE
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author-letter	Alekhova, E. Yu.
doi_str_mv	10.3103/S0025654408030060
dewey-full	600
title_sort	mathematical model of the sensor unit for processing on-board algorithms of navigation systems
title_auth	Mathematical model of the sensor unit for processing on-board algorithms of navigation systems
abstract	Abstract Recently, strapdown gyro navigation systems have become widely used. In such systems, sensors, gyros, and accelerometers are placed directly aboard the object and an imaginary analytic trihedral is used instead of a stabilized gyroplatform. The object orientation with respect to the analytic trihedral is calculated by numerically solving the Poisson equations taking into account the readings of gyro sensors measuring the object angular velocities. The mutual orientation parameters permit recalculating the apparent acceleration measured by the accelerometers on the object axes for the axes of the analytic trihedral. In the analytic trihedral, the navigation problem is solved in the same way as it is solved in platform systems but, in the whole, the functions of the onboard algorithms of strapdown systems are significantly more complicated than those of platform systems. The possibility of detailed processing of on-board algorithms is of great importance for ensuring the accuracy of the entire navigation system. In the present paper, we state algorithms for reproducing the exact readings of ideal gyro sensors and the exact readings of ideal accelerometers under bench operating conditions of the system under an angular motion imitating the object orientation evolution and the possible angular vibration. Simultaneously, we calculate the exact position and orientation parameters, which can be compared with the results produced by the on-board algorithm.
abstractGer	Abstract Recently, strapdown gyro navigation systems have become widely used. In such systems, sensors, gyros, and accelerometers are placed directly aboard the object and an imaginary analytic trihedral is used instead of a stabilized gyroplatform. The object orientation with respect to the analytic trihedral is calculated by numerically solving the Poisson equations taking into account the readings of gyro sensors measuring the object angular velocities. The mutual orientation parameters permit recalculating the apparent acceleration measured by the accelerometers on the object axes for the axes of the analytic trihedral. In the analytic trihedral, the navigation problem is solved in the same way as it is solved in platform systems but, in the whole, the functions of the onboard algorithms of strapdown systems are significantly more complicated than those of platform systems. The possibility of detailed processing of on-board algorithms is of great importance for ensuring the accuracy of the entire navigation system. In the present paper, we state algorithms for reproducing the exact readings of ideal gyro sensors and the exact readings of ideal accelerometers under bench operating conditions of the system under an angular motion imitating the object orientation evolution and the possible angular vibration. Simultaneously, we calculate the exact position and orientation parameters, which can be compared with the results produced by the on-board algorithm.
abstract_unstemmed	Abstract Recently, strapdown gyro navigation systems have become widely used. In such systems, sensors, gyros, and accelerometers are placed directly aboard the object and an imaginary analytic trihedral is used instead of a stabilized gyroplatform. The object orientation with respect to the analytic trihedral is calculated by numerically solving the Poisson equations taking into account the readings of gyro sensors measuring the object angular velocities. The mutual orientation parameters permit recalculating the apparent acceleration measured by the accelerometers on the object axes for the axes of the analytic trihedral. In the analytic trihedral, the navigation problem is solved in the same way as it is solved in platform systems but, in the whole, the functions of the onboard algorithms of strapdown systems are significantly more complicated than those of platform systems. The possibility of detailed processing of on-board algorithms is of great importance for ensuring the accuracy of the entire navigation system. In the present paper, we state algorithms for reproducing the exact readings of ideal gyro sensors and the exact readings of ideal accelerometers under bench operating conditions of the system under an angular motion imitating the object orientation evolution and the possible angular vibration. Simultaneously, we calculate the exact position and orientation parameters, which can be compared with the results produced by the on-board algorithm.
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title_short	Mathematical model of the sensor unit for processing on-board algorithms of navigation systems
url	https://dx.doi.org/10.3103/S0025654408030060
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doi_str	10.3103/S0025654408030060
up_date	2024-07-03T17:49:24.031Z
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Yu.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Mathematical model of the sensor unit for processing on-board algorithms of navigation systems</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2008</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract Recently, strapdown gyro navigation systems have become widely used. In such systems, sensors, gyros, and accelerometers are placed directly aboard the object and an imaginary analytic trihedral is used instead of a stabilized gyroplatform. The object orientation with respect to the analytic trihedral is calculated by numerically solving the Poisson equations taking into account the readings of gyro sensors measuring the object angular velocities. The mutual orientation parameters permit recalculating the apparent acceleration measured by the accelerometers on the object axes for the axes of the analytic trihedral. In the analytic trihedral, the navigation problem is solved in the same way as it is solved in platform systems but, in the whole, the functions of the onboard algorithms of strapdown systems are significantly more complicated than those of platform systems. The possibility of detailed processing of on-board algorithms is of great importance for ensuring the accuracy of the entire navigation system. In the present paper, we state algorithms for reproducing the exact readings of ideal gyro sensors and the exact readings of ideal accelerometers under bench operating conditions of the system under an angular motion imitating the object orientation evolution and the possible angular vibration. 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