Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation
This paper investigates the attitude control of a modular picosatellite named NPU-PhoneSat based on shape actuation. The PhoneSat is composed of multiple blocks connected by active joints. Much like a falling cat can reorient itself in mid-air, this modular PhoneSat could reorient itself without cha...
Ausführliche Beschreibung
Autor*in: |
Qiao, Qiao [verfasserIn] Yuan, Jianping [verfasserIn] Wang, Mingming [verfasserIn] Ning, Xin [verfasserIn] |
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Format: |
E-Artikel |
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Sprache: |
Englisch |
Erschienen: |
2017 |
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Schlagwörter: |
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Übergeordnetes Werk: |
Enthalten in: Aerospace science and technology - Amsterdam [u.a.] : Elsevier Science, 1997, 71, Seite 62-67 |
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Übergeordnetes Werk: |
volume:71 ; pages:62-67 |
DOI / URN: |
10.1016/j.ast.2017.09.011 |
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Katalog-ID: |
ELV000609153 |
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245 | 1 | 0 | |a Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation |
264 | 1 | |c 2017 | |
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520 | |a This paper investigates the attitude control of a modular picosatellite named NPU-PhoneSat based on shape actuation. The PhoneSat is composed of multiple blocks connected by active joints. Much like a falling cat can reorient itself in mid-air, this modular PhoneSat could reorient itself without changes in net angular momentum by altering the shape and instantaneous mass distribution during attitude maneuvers. Given size and cost constraints, the number of actuators should be limited. Thus, this paper focuses on the under-actuated case. Optimal attitude control method to steer the PhoneSat to the desired posture is proposed in this paper. The inequality constraints are established based on the capacity of the actuator. Particle Swarm Optimization algorithm is employed to search the optimal control input to achieve the reorientation while satisfying the imposed constraints. The input torque is parameterized by the spline to guarantee that initial and final values of control input are zero. Simulation results of zero-angular-momentum reorientation of the PhoneSat are presented which confirm the effectiveness of the proposed method. | ||
650 | 4 | |a PhoneSat | |
650 | 4 | |a Shape actuation | |
650 | 4 | |a Attitude control | |
650 | 4 | |a Particle swarm optimization | |
700 | 1 | |a Yuan, Jianping |e verfasserin |4 aut | |
700 | 1 | |a Wang, Mingming |e verfasserin |4 aut | |
700 | 1 | |a Ning, Xin |e verfasserin |4 aut | |
773 | 0 | 8 | |i Enthalten in |t Aerospace science and technology |d Amsterdam [u.a.] : Elsevier Science, 1997 |g 71, Seite 62-67 |h Online-Ressource |w (DE-627)320521486 |w (DE-600)2014638-3 |w (DE-576)255630425 |x 1626-3219 |7 nnns |
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936 | b | k | |a 55.50 |j Luftfahrzeugtechnik |
936 | b | k | |a 55.60 |j Raumfahrttechnik |
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2017 |
allfields |
10.1016/j.ast.2017.09.011 doi (DE-627)ELV000609153 (ELSEVIER)S1270-9638(16)30270-X DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Qiao, Qiao verfasserin aut Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation 2017 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper investigates the attitude control of a modular picosatellite named NPU-PhoneSat based on shape actuation. The PhoneSat is composed of multiple blocks connected by active joints. Much like a falling cat can reorient itself in mid-air, this modular PhoneSat could reorient itself without changes in net angular momentum by altering the shape and instantaneous mass distribution during attitude maneuvers. Given size and cost constraints, the number of actuators should be limited. Thus, this paper focuses on the under-actuated case. Optimal attitude control method to steer the PhoneSat to the desired posture is proposed in this paper. The inequality constraints are established based on the capacity of the actuator. Particle Swarm Optimization algorithm is employed to search the optimal control input to achieve the reorientation while satisfying the imposed constraints. The input torque is parameterized by the spline to guarantee that initial and final values of control input are zero. Simulation results of zero-angular-momentum reorientation of the PhoneSat are presented which confirm the effectiveness of the proposed method. PhoneSat Shape actuation Attitude control Particle swarm optimization Yuan, Jianping verfasserin aut Wang, Mingming verfasserin aut Ning, Xin verfasserin aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 71, Seite 62-67 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:71 pages:62-67 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_34 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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 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_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_2056 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_2098 GBV_ILN_2106 GBV_ILN_2108 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_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 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_4338 GBV_ILN_4393 55.50 Luftfahrzeugtechnik 55.60 Raumfahrttechnik 55.60 Raumfahrttechnik AR 71 62-67 |
spelling |
10.1016/j.ast.2017.09.011 doi (DE-627)ELV000609153 (ELSEVIER)S1270-9638(16)30270-X DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Qiao, Qiao verfasserin aut Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation 2017 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper investigates the attitude control of a modular picosatellite named NPU-PhoneSat based on shape actuation. The PhoneSat is composed of multiple blocks connected by active joints. Much like a falling cat can reorient itself in mid-air, this modular PhoneSat could reorient itself without changes in net angular momentum by altering the shape and instantaneous mass distribution during attitude maneuvers. Given size and cost constraints, the number of actuators should be limited. Thus, this paper focuses on the under-actuated case. Optimal attitude control method to steer the PhoneSat to the desired posture is proposed in this paper. The inequality constraints are established based on the capacity of the actuator. Particle Swarm Optimization algorithm is employed to search the optimal control input to achieve the reorientation while satisfying the imposed constraints. The input torque is parameterized by the spline to guarantee that initial and final values of control input are zero. Simulation results of zero-angular-momentum reorientation of the PhoneSat are presented which confirm the effectiveness of the proposed method. PhoneSat Shape actuation Attitude control Particle swarm optimization Yuan, Jianping verfasserin aut Wang, Mingming verfasserin aut Ning, Xin verfasserin aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 71, Seite 62-67 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:71 pages:62-67 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_34 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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 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_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_2056 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_2098 GBV_ILN_2106 GBV_ILN_2108 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_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 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_4338 GBV_ILN_4393 55.50 Luftfahrzeugtechnik 55.60 Raumfahrttechnik 55.60 Raumfahrttechnik AR 71 62-67 |
allfields_unstemmed |
10.1016/j.ast.2017.09.011 doi (DE-627)ELV000609153 (ELSEVIER)S1270-9638(16)30270-X DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Qiao, Qiao verfasserin aut Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation 2017 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper investigates the attitude control of a modular picosatellite named NPU-PhoneSat based on shape actuation. The PhoneSat is composed of multiple blocks connected by active joints. Much like a falling cat can reorient itself in mid-air, this modular PhoneSat could reorient itself without changes in net angular momentum by altering the shape and instantaneous mass distribution during attitude maneuvers. Given size and cost constraints, the number of actuators should be limited. Thus, this paper focuses on the under-actuated case. Optimal attitude control method to steer the PhoneSat to the desired posture is proposed in this paper. The inequality constraints are established based on the capacity of the actuator. Particle Swarm Optimization algorithm is employed to search the optimal control input to achieve the reorientation while satisfying the imposed constraints. The input torque is parameterized by the spline to guarantee that initial and final values of control input are zero. Simulation results of zero-angular-momentum reorientation of the PhoneSat are presented which confirm the effectiveness of the proposed method. PhoneSat Shape actuation Attitude control Particle swarm optimization Yuan, Jianping verfasserin aut Wang, Mingming verfasserin aut Ning, Xin verfasserin aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 71, Seite 62-67 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:71 pages:62-67 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_34 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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 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_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_2056 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_2098 GBV_ILN_2106 GBV_ILN_2108 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_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 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_4338 GBV_ILN_4393 55.50 Luftfahrzeugtechnik 55.60 Raumfahrttechnik 55.60 Raumfahrttechnik AR 71 62-67 |
allfieldsGer |
10.1016/j.ast.2017.09.011 doi (DE-627)ELV000609153 (ELSEVIER)S1270-9638(16)30270-X DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Qiao, Qiao verfasserin aut Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation 2017 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper investigates the attitude control of a modular picosatellite named NPU-PhoneSat based on shape actuation. The PhoneSat is composed of multiple blocks connected by active joints. Much like a falling cat can reorient itself in mid-air, this modular PhoneSat could reorient itself without changes in net angular momentum by altering the shape and instantaneous mass distribution during attitude maneuvers. Given size and cost constraints, the number of actuators should be limited. Thus, this paper focuses on the under-actuated case. Optimal attitude control method to steer the PhoneSat to the desired posture is proposed in this paper. The inequality constraints are established based on the capacity of the actuator. Particle Swarm Optimization algorithm is employed to search the optimal control input to achieve the reorientation while satisfying the imposed constraints. The input torque is parameterized by the spline to guarantee that initial and final values of control input are zero. Simulation results of zero-angular-momentum reorientation of the PhoneSat are presented which confirm the effectiveness of the proposed method. PhoneSat Shape actuation Attitude control Particle swarm optimization Yuan, Jianping verfasserin aut Wang, Mingming verfasserin aut Ning, Xin verfasserin aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 71, Seite 62-67 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:71 pages:62-67 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_34 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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 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_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_2056 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_2098 GBV_ILN_2106 GBV_ILN_2108 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_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 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_4338 GBV_ILN_4393 55.50 Luftfahrzeugtechnik 55.60 Raumfahrttechnik 55.60 Raumfahrttechnik AR 71 62-67 |
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10.1016/j.ast.2017.09.011 doi (DE-627)ELV000609153 (ELSEVIER)S1270-9638(16)30270-X DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Qiao, Qiao verfasserin aut Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation 2017 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper investigates the attitude control of a modular picosatellite named NPU-PhoneSat based on shape actuation. The PhoneSat is composed of multiple blocks connected by active joints. Much like a falling cat can reorient itself in mid-air, this modular PhoneSat could reorient itself without changes in net angular momentum by altering the shape and instantaneous mass distribution during attitude maneuvers. Given size and cost constraints, the number of actuators should be limited. Thus, this paper focuses on the under-actuated case. Optimal attitude control method to steer the PhoneSat to the desired posture is proposed in this paper. The inequality constraints are established based on the capacity of the actuator. Particle Swarm Optimization algorithm is employed to search the optimal control input to achieve the reorientation while satisfying the imposed constraints. The input torque is parameterized by the spline to guarantee that initial and final values of control input are zero. Simulation results of zero-angular-momentum reorientation of the PhoneSat are presented which confirm the effectiveness of the proposed method. PhoneSat Shape actuation Attitude control Particle swarm optimization Yuan, Jianping verfasserin aut Wang, Mingming verfasserin aut Ning, Xin verfasserin aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 71, Seite 62-67 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:71 pages:62-67 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_34 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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 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_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_2056 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_2098 GBV_ILN_2106 GBV_ILN_2108 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_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 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_4338 GBV_ILN_4393 55.50 Luftfahrzeugtechnik 55.60 Raumfahrttechnik 55.60 Raumfahrttechnik AR 71 62-67 |
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Qiao, Qiao @@aut@@ Yuan, Jianping @@aut@@ Wang, Mingming @@aut@@ Ning, Xin @@aut@@ |
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Qiao, Qiao |
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Qiao, Qiao ddc 620 bkl 55.50 bkl 55.60 misc PhoneSat misc Shape actuation misc Attitude control misc Particle swarm optimization Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation |
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620 DE-600 55.50 bkl 55.60 bkl Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation PhoneSat Shape actuation Attitude control Particle swarm optimization |
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ddc 620 bkl 55.50 bkl 55.60 misc PhoneSat misc Shape actuation misc Attitude control misc Particle swarm optimization |
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Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation |
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attitude control of a picosatellite named npu-phonesat based on shape actuation |
title_auth |
Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation |
abstract |
This paper investigates the attitude control of a modular picosatellite named NPU-PhoneSat based on shape actuation. The PhoneSat is composed of multiple blocks connected by active joints. Much like a falling cat can reorient itself in mid-air, this modular PhoneSat could reorient itself without changes in net angular momentum by altering the shape and instantaneous mass distribution during attitude maneuvers. Given size and cost constraints, the number of actuators should be limited. Thus, this paper focuses on the under-actuated case. Optimal attitude control method to steer the PhoneSat to the desired posture is proposed in this paper. The inequality constraints are established based on the capacity of the actuator. Particle Swarm Optimization algorithm is employed to search the optimal control input to achieve the reorientation while satisfying the imposed constraints. The input torque is parameterized by the spline to guarantee that initial and final values of control input are zero. Simulation results of zero-angular-momentum reorientation of the PhoneSat are presented which confirm the effectiveness of the proposed method. |
abstractGer |
This paper investigates the attitude control of a modular picosatellite named NPU-PhoneSat based on shape actuation. The PhoneSat is composed of multiple blocks connected by active joints. Much like a falling cat can reorient itself in mid-air, this modular PhoneSat could reorient itself without changes in net angular momentum by altering the shape and instantaneous mass distribution during attitude maneuvers. Given size and cost constraints, the number of actuators should be limited. Thus, this paper focuses on the under-actuated case. Optimal attitude control method to steer the PhoneSat to the desired posture is proposed in this paper. The inequality constraints are established based on the capacity of the actuator. Particle Swarm Optimization algorithm is employed to search the optimal control input to achieve the reorientation while satisfying the imposed constraints. The input torque is parameterized by the spline to guarantee that initial and final values of control input are zero. Simulation results of zero-angular-momentum reorientation of the PhoneSat are presented which confirm the effectiveness of the proposed method. |
abstract_unstemmed |
This paper investigates the attitude control of a modular picosatellite named NPU-PhoneSat based on shape actuation. The PhoneSat is composed of multiple blocks connected by active joints. Much like a falling cat can reorient itself in mid-air, this modular PhoneSat could reorient itself without changes in net angular momentum by altering the shape and instantaneous mass distribution during attitude maneuvers. Given size and cost constraints, the number of actuators should be limited. Thus, this paper focuses on the under-actuated case. Optimal attitude control method to steer the PhoneSat to the desired posture is proposed in this paper. The inequality constraints are established based on the capacity of the actuator. Particle Swarm Optimization algorithm is employed to search the optimal control input to achieve the reorientation while satisfying the imposed constraints. The input torque is parameterized by the spline to guarantee that initial and final values of control input are zero. Simulation results of zero-angular-momentum reorientation of the PhoneSat are presented which confirm the effectiveness of the proposed method. |
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Attitude control of a picosatellite named NPU-PhoneSat based on shape actuation |
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|
score |
7.397662 |