Experimental verification and comparison of fuzzy and PID controllers for attitude control of nanosatellites
•Experimental comparison on ground of Fuzzy and PID attitude controllers for nanosatellites.•The fuzzy controller provides advantages in energy and convergence time.•Their lower energy consumption makes fuzzy controllers more suitable for nanosatellite missions. Modern control algorithms based on ar...
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| Published in | Advances in space research Vol. 71; no. 9; pp. 3613 - 3630 |
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| Main Authors | , , , , |
| Format | Journal Article |
| Language | English |
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Elsevier B.V
01.05.2023
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| Subjects | |
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| Abstract | •Experimental comparison on ground of Fuzzy and PID attitude controllers for nanosatellites.•The fuzzy controller provides advantages in energy and convergence time.•Their lower energy consumption makes fuzzy controllers more suitable for nanosatellite missions.
Modern control algorithms based on artificial intelligence have shown good results in many application fields. That is why some researchers have made an effort to introduce them in the attitude control of satellites by computing their performance in simulated scenarios. However, there is a lack of experimental data due to the cost and inherent risk of testing new attitude control algorithms on board a real satellite. In this work, a laboratory nanosatellite and its testing system have been used to experimentally compare the performance of a fuzzy logic controller, a classical Proportional Integral and Derivative (PID) controller and a modified PID. Comparisons have been drawn in terms of energy consumption, convergence time, accuracy (steady state error) and robustness (with respect to variations in the external conditions). In line with previous numerical studies, the results suggest significant improvements in energy consumption, convergence time and robustness by using a fuzzy controller instead of a PID. |
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| AbstractList | •Experimental comparison on ground of Fuzzy and PID attitude controllers for nanosatellites.•The fuzzy controller provides advantages in energy and convergence time.•Their lower energy consumption makes fuzzy controllers more suitable for nanosatellite missions.
Modern control algorithms based on artificial intelligence have shown good results in many application fields. That is why some researchers have made an effort to introduce them in the attitude control of satellites by computing their performance in simulated scenarios. However, there is a lack of experimental data due to the cost and inherent risk of testing new attitude control algorithms on board a real satellite. In this work, a laboratory nanosatellite and its testing system have been used to experimentally compare the performance of a fuzzy logic controller, a classical Proportional Integral and Derivative (PID) controller and a modified PID. Comparisons have been drawn in terms of energy consumption, convergence time, accuracy (steady state error) and robustness (with respect to variations in the external conditions). In line with previous numerical studies, the results suggest significant improvements in energy consumption, convergence time and robustness by using a fuzzy controller instead of a PID. |
| Author | Ezquerro, J.M. Bello, A. Rodríguez, J. Olfe, K.S. Lapuerta, V. |
| Author_xml | – sequence: 1 givenname: A. surname: Bello fullname: Bello, A. email: alvaro.bello@upm.es – sequence: 2 givenname: K.S. surname: Olfe fullname: Olfe, K.S. email: kolfe@eusoc.upm.es – sequence: 3 givenname: J. surname: Rodríguez fullname: Rodríguez, J. email: jacobo.rodriguez@upm.es – sequence: 4 givenname: J.M. surname: Ezquerro fullname: Ezquerro, J.M. email: jm.ezquerro@upm.es – sequence: 5 givenname: V. surname: Lapuerta fullname: Lapuerta, V. email: mariavictoria.lapuerta@upm.es |
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| Keywords | Fuzzy logic Attitude control Nanosatellites Artificial intelligence |
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| References | Castillo, Cervantes, Soria, Sanchez, Castro (b0035) 2016; 354 Keat, J.E., 1977. Analysis of Least-Squares Attitude Determination Routine DOAOP, Computer Sciences Corporation. Ousaloo (b0140) 2019; 157 Cervantes, Castillo (b0040) 2015; 324 Ziegler, Nichols (b0215) 1993; 115 Mukherjee, Giri, Sinha (b0120) 2017; 54 Kim, Kim (b0095) 2001; 24 Gaber, El_Mashade, Aziz (b0085) 2020; 85 Liu, Guo, Zhang (b0105) 2012; 67 Favarim, F., Cris Brito, R., Linares, K.S.C., Todt, E., 2018. Comparison analysis between PID and fuzzy logic controllers for quadrotor in a simulated and in a real environment, in: Proceedings - 15th Latin American Robotics Symposium, 6th Brazilian Robotics Symposium and 9th Workshop on Robotics in Education, LARS/SBR/WRE 2018. pp. 490–495. Sendi (b0170) 2022; 10 Conti, Souza (b0060) 2008; 15 Mahdi (b0110) 2016; 4 Millan, von Steiger, Ariel, Bartalev, Borgeaud, Campagnola, Castillo-Rogez, Fléron, Gass, Gregorio, Klumpar, Lal, Macdonald, Park, Sambasiva Rao, Schilling, Stephens, Title, Wu (b0115) 2019; 64 Souza, Gonzáles (b0180) 2012; 19 QB50 project [WWW Document], n.d. URL Najafizadeh Sari, Jahanshahi, Fakoor (b0130) 2019; 21 Theia Space [WWW Document], n.d. URL Sweeting, M.N., 2018. Modern Small Satellites-Changing the Economics of Space, in: Proceedings of the IEEE. pp. 343–361. Kim, Park, Park (b0100) 2016; 57 OPS-SAT [WWW Document], n.d. URL Chen, Zhong, Liu, Cong (b0050) 2016; 18 Salgado Sánchez, López-Fernández, Fernández, Ezquerro, Rodríguez, Del Cura, Lapuerta (b0160) 2021; 1 Bernardes, de Farias, Rodrigues, Murilo, Lopes, Avila (b0020) 2019; 7 Bello, Á., Olfe, K., Ezquerro, J.M., Rodríguez, J., Lapuerta, V., 2019. Experimental comparison of attitude controllers for nanosatellites, in: 8TH European Conference for Aeronautics and Space Sciences (EUCASS). pp. EUCASS2019-386 (1–15). Bello, del Castañedo, Stephan Olfe, Rodríguez, Lapuerta (b0010) 2021; 174 Murilo, de Deus Peixoto, Gadelha de Souza, Lopes (b0125) 2021; 149 Cheng, Shu, Cheng (b0055) 2009; 36 E-USOC [WWW Document], n.d. URL Ousaloo, Nodeh, Mehrabian (b0145) 2016; 126 De Souza (b0065) 2006; 34 Walker, Putman, Cohen (b0195) 2015; 52 . Chak, Varatharajoo, Assadian (b0045) 2021; 93 Diebel (b0070) 2006; 58 Wang, Abtahi, Chahari (b0200) 2022; 10 Calvo, Bello, Lapuerta, Laverón-Simavilla (b0030) 2018 Zeghlache, Benslimane, Amardjia, Bouguerra (b0210) 2017; 19 Polo, Esteban, Cercos, Parra, Angulo (b0150) 2014; 93 Calvo, Avilés, Lapuerta, Laverón-Simavilla (b0025) 2016; 58 Schwartz, Peck, Hall (b0165) 2003; 26 Yadegari, Beyramzad, Khanmirza (b0205) 2022; 69 Ahmed, Mashor, Mahdi (b0005) 2019 Sidi, M.J., 2014. Spacecraft dynamics and control: A practical engineering approach, Cambridge University Press. Cambridge. Ousaloo (10.1016/j.asr.2022.05.055_b0140) 2019; 157 Diebel (10.1016/j.asr.2022.05.055_b0070) 2006; 58 10.1016/j.asr.2022.05.055_b0185 Bello (10.1016/j.asr.2022.05.055_b0010) 2021; 174 Bernardes (10.1016/j.asr.2022.05.055_b0020) 2019; 7 Mukherjee (10.1016/j.asr.2022.05.055_b0120) 2017; 54 10.1016/j.asr.2022.05.055_b0080 Ousaloo (10.1016/j.asr.2022.05.055_b0145) 2016; 126 Mahdi (10.1016/j.asr.2022.05.055_b0110) 2016; 4 Ahmed (10.1016/j.asr.2022.05.055_b0005) 2019 Polo (10.1016/j.asr.2022.05.055_b0150) 2014; 93 Kim (10.1016/j.asr.2022.05.055_b0100) 2016; 57 Kim (10.1016/j.asr.2022.05.055_b0095) 2001; 24 Castillo (10.1016/j.asr.2022.05.055_b0035) 2016; 354 Millan (10.1016/j.asr.2022.05.055_b0115) 2019; 64 Wang (10.1016/j.asr.2022.05.055_b0200) 2022; 10 Yadegari (10.1016/j.asr.2022.05.055_b0205) 2022; 69 Gaber (10.1016/j.asr.2022.05.055_b0085) 2020; 85 Salgado Sánchez (10.1016/j.asr.2022.05.055_b0160) 2021; 1 Ziegler (10.1016/j.asr.2022.05.055_b0215) 1993; 115 Calvo (10.1016/j.asr.2022.05.055_b0030) 2018 Cheng (10.1016/j.asr.2022.05.055_b0055) 2009; 36 10.1016/j.asr.2022.05.055_b0135 10.1016/j.asr.2022.05.055_b0155 10.1016/j.asr.2022.05.055_b0075 10.1016/j.asr.2022.05.055_b0175 De Souza (10.1016/j.asr.2022.05.055_b0065) 2006; 34 Murilo (10.1016/j.asr.2022.05.055_b0125) 2021; 149 Walker (10.1016/j.asr.2022.05.055_b0195) 2015; 52 10.1016/j.asr.2022.05.055_b0190 10.1016/j.asr.2022.05.055_b0090 Conti (10.1016/j.asr.2022.05.055_b0060) 2008; 15 Liu (10.1016/j.asr.2022.05.055_b0105) 2012; 67 Schwartz (10.1016/j.asr.2022.05.055_b0165) 2003; 26 Sendi (10.1016/j.asr.2022.05.055_b0170) 2022; 10 Najafizadeh Sari (10.1016/j.asr.2022.05.055_b0130) 2019; 21 Cervantes (10.1016/j.asr.2022.05.055_b0040) 2015; 324 Calvo (10.1016/j.asr.2022.05.055_b0025) 2016; 58 Souza (10.1016/j.asr.2022.05.055_b0180) 2012; 19 Chak (10.1016/j.asr.2022.05.055_b0045) 2021; 93 10.1016/j.asr.2022.05.055_b0015 Chen (10.1016/j.asr.2022.05.055_b0050) 2016; 18 Zeghlache (10.1016/j.asr.2022.05.055_b0210) 2017; 19 |
| References_xml | – volume: 57 start-page: 137 year: 2016 end-page: 152 ident: b0100 article-title: Spacecraft attitude control using neuro-fuzzy approximation of the optimal controllers publication-title: Adv. Sp. Res. contributor: fullname: Park – volume: 149 start-page: 107129 year: 2021 ident: b0125 article-title: Real-time implementation of a parameterized Model Predictive Control for Attitude Control Systems of rigid-flexible satellite publication-title: Mech. Syst. Signal Process. contributor: fullname: Lopes – volume: 115 start-page: 220 year: 1993 end-page: 222 ident: b0215 article-title: Optimum settings for automatic controllers publication-title: J. Dyn. Syst. Meas. Control. Trans. ASME contributor: fullname: Nichols – volume: 64 start-page: 1466 year: 2019 end-page: 1517 ident: b0115 article-title: Small satellites for space science: A COSPAR scientific roadmap publication-title: Adv. Sp. Res. contributor: fullname: Wu – volume: 54 start-page: 1 year: 2017 end-page: 8 ident: b0120 article-title: Lorentz-force-based fuzzy proportional-integral-derivative attitude control for earth-pointing satellites publication-title: J. Spacecr. Rockets contributor: fullname: Sinha – volume: 324 start-page: 247 year: 2015 end-page: 256 ident: b0040 article-title: Type-2 fuzzy logic aggregation of multiple fuzzy controllers for airplane flight control publication-title: Inf. Sci. (Ny) contributor: fullname: Castillo – volume: 15 start-page: 395 year: 2008 end-page: 402 ident: b0060 article-title: Satellite attitude control system simulator publication-title: Shock Vib. contributor: fullname: Souza – volume: 52 start-page: 1627 year: 2015 end-page: 1639 ident: b0195 article-title: Solely magnetic genetic/fuzzy-attitude-control algorithm for a CubeSat publication-title: J. Spacecr. Rockets contributor: fullname: Cohen – volume: 69 start-page: 3204 year: 2022 end-page: 3225 ident: b0205 article-title: Magnetorquers-based satellite attitude control using interval type-II fuzzy terminal sliding mode control with time delay estimation publication-title: Adv. Sp. Res. contributor: fullname: Khanmirza – volume: 36 start-page: 6613 year: 2009 end-page: 6620 ident: b0055 article-title: Attitude control of a satellite using fuzzy controllers publication-title: Expert Syst. Appl. contributor: fullname: Cheng – volume: 4 start-page: 407 year: 2016 end-page: 416 ident: b0110 article-title: Fuzzy Pid Controller for Nano-Satellite Attitude Control publication-title: J. Sci. Arts contributor: fullname: Mahdi – volume: 93 start-page: 94 year: 2014 end-page: 105 ident: b0150 article-title: End-to-end validation process for the INTA-Nanosat-1B Attitude Control System publication-title: Acta Astronaut. contributor: fullname: Angulo – volume: 18 start-page: 631 year: 2016 end-page: 641 ident: b0050 article-title: Adaptive Fuzzy PD+ Control for Attitude Maneuver of Rigid Spacecraft publication-title: Asian J. Control contributor: fullname: Cong – start-page: 1 year: 2018 end-page: 9 ident: b0030 article-title: Comparison of fuzzy and pid controllers for the attitude control of nanosatellites publication-title: Adv. Intell. Syst. Comput. contributor: fullname: Laverón-Simavilla – volume: 19 year: 2012 ident: b0180 article-title: Application of the state-dependent riccati equation and kalman filter techniques to the design of a satellite control system publication-title: Shock Vib. contributor: fullname: Gonzáles – volume: 58 start-page: 1 year: 2006 end-page: 35 ident: b0070 article-title: Representing attitude: Euler angles, unit quaternions, and rotation vectors publication-title: Matrix contributor: fullname: Diebel – volume: 10 start-page: 179 year: 2022 ident: b0170 article-title: Attitude Control of a Flexible Spacecraft via Fuzzy Optimal Variance Technique publication-title: Mathematics contributor: fullname: Sendi – volume: 1 start-page: 2581 year: 2021 end-page: 2586 ident: b0160 article-title: Challenge-Based Learning and Concurrent Engineering in Aerospace Engineering Education publication-title: INTED2021 Proc. contributor: fullname: Lapuerta – volume: 24 start-page: 1 year: 2001 end-page: 18 ident: b0095 article-title: Spin-axis stabilization of a rigid spacecraft using two reaction wheels publication-title: J. Guid. Control. Dyn. contributor: fullname: Kim – volume: 93 start-page: 1 year: 2021 end-page: 14 ident: b0045 article-title: Adaptive fuzzy Jacobian control of spacecraft combined attitude and Sun tracking system publication-title: Aircr. Eng. Aerosp. Technol. contributor: fullname: Assadian – volume: 34 start-page: 351 year: 2006 end-page: 364 ident: b0065 article-title: Design of satellite control system using optimal nonlinear theory publication-title: Mech. Based Des. Struct. Mach. contributor: fullname: De Souza – volume: 67 start-page: 2081 year: 2012 end-page: 2088 ident: b0105 article-title: An anti-disturbance PD control scheme for attitude control and stabilization of flexible spacecrafts publication-title: Nonlinear Dyn. contributor: fullname: Zhang – volume: 174 start-page: 114679 year: 2021 ident: b0010 article-title: Parameterized fuzzy-logic controllers for the attitude control of nanosatellites in low earth orbits. A comparative studio with PID controllers publication-title: Expert Syst. Appl. contributor: fullname: Lapuerta – volume: 7 start-page: 111499 year: 2019 end-page: 111512 ident: b0020 article-title: Low-cost hardware-in-the-loop platform for embedded control strategies simulation publication-title: IEEE Access contributor: fullname: Avila – start-page: 1372 year: 2019 ident: b0005 article-title: Intelligent Fuzzy PD+I Controller with Stabilizer for Nano Satellite Attitude Control System publication-title: J. Phys. Conf. Ser. contributor: fullname: Mahdi – volume: 157 start-page: 17 year: 2019 end-page: 28 ident: b0140 article-title: Globally asymptotic three-axis attitude control for a two-wheeled small satellite publication-title: Acta Astronaut. contributor: fullname: Ousaloo – volume: 21 start-page: 768 year: 2019 end-page: 781 ident: b0130 article-title: Adaptive Fuzzy PID Control Strategy for Spacecraft Attitude Control publication-title: Int. J. Fuzzy Syst. contributor: fullname: Fakoor – volume: 26 start-page: 513 year: 2003 end-page: 522 ident: b0165 article-title: Historical review of air-bearing spacecraft simulators publication-title: J. Guid. Control. Dyn. contributor: fullname: Hall – volume: 10 start-page: 976 year: 2022 ident: b0200 article-title: An Adaptive Neuro-Fuzzy Model for Attitude Estimation and Control of a 3 DOF System publication-title: Mathematics contributor: fullname: Chahari – volume: 354 start-page: 165 year: 2016 end-page: 177 ident: b0035 article-title: A generalized type-2 fuzzy granular approach with applications to aerospace publication-title: Inf. Sci. (Ny) contributor: fullname: Castro – volume: 19 start-page: 1444 year: 2017 end-page: 1463 ident: b0210 article-title: Interval Type-2 Fuzzy Sliding Mode Controller Based on Nonlinear Observer for a 3-DOF Helicopter with Uncertainties publication-title: Int. J. Fuzzy Syst. contributor: fullname: Bouguerra – volume: 58 start-page: 102 year: 2016 end-page: 118 ident: b0025 article-title: Fuzzy attitude control for a nanosatellite in low Earth orbit publication-title: Expert Syst. Appl. contributor: fullname: Laverón-Simavilla – volume: 85 start-page: 106679 year: 2020 ident: b0085 article-title: Hardware-in-the-loop real-time validation of micro-satellite attitude control publication-title: Comput. Electr. Eng. contributor: fullname: Aziz – volume: 126 start-page: 546 year: 2016 end-page: 553 ident: b0145 article-title: Verification of Spin Magnetic Attitude Control System using air-bearing-based attitude control simulator publication-title: Acta Astronaut. contributor: fullname: Mehrabian – volume: 18 start-page: 631 year: 2016 ident: 10.1016/j.asr.2022.05.055_b0050 article-title: Adaptive Fuzzy PD+ Control for Attitude Maneuver of Rigid Spacecraft publication-title: Asian J. Control doi: 10.1002/asjc.1116 contributor: fullname: Chen – ident: 10.1016/j.asr.2022.05.055_b0185 doi: 10.1109/JPROC.2018.2806218 – ident: 10.1016/j.asr.2022.05.055_b0135 – volume: 15 start-page: 395 year: 2008 ident: 10.1016/j.asr.2022.05.055_b0060 article-title: Satellite attitude control system simulator publication-title: Shock Vib. doi: 10.1155/2008/141465 contributor: fullname: Conti – volume: 174 start-page: 114679 issue: 1–28 year: 2021 ident: 10.1016/j.asr.2022.05.055_b0010 article-title: Parameterized fuzzy-logic controllers for the attitude control of nanosatellites in low earth orbits. A comparative studio with PID controllers publication-title: Expert Syst. Appl. doi: 10.1016/j.eswa.2021.114679 contributor: fullname: Bello – volume: 157 start-page: 17 year: 2019 ident: 10.1016/j.asr.2022.05.055_b0140 article-title: Globally asymptotic three-axis attitude control for a two-wheeled small satellite publication-title: Acta Astronaut. doi: 10.1016/j.actaastro.2018.11.055 contributor: fullname: Ousaloo – volume: 93 start-page: 94 year: 2014 ident: 10.1016/j.asr.2022.05.055_b0150 article-title: End-to-end validation process for the INTA-Nanosat-1B Attitude Control System publication-title: Acta Astronaut. doi: 10.1016/j.actaastro.2013.07.001 contributor: fullname: Polo – volume: 324 start-page: 247 year: 2015 ident: 10.1016/j.asr.2022.05.055_b0040 article-title: Type-2 fuzzy logic aggregation of multiple fuzzy controllers for airplane flight control publication-title: Inf. Sci. (Ny) doi: 10.1016/j.ins.2015.06.047 contributor: fullname: Cervantes – volume: 24 start-page: 1 year: 2001 ident: 10.1016/j.asr.2022.05.055_b0095 article-title: Spin-axis stabilization of a rigid spacecraft using two reaction wheels publication-title: J. Guid. Control. Dyn. doi: 10.2514/2.4818 contributor: fullname: Kim – volume: 26 start-page: 513 year: 2003 ident: 10.1016/j.asr.2022.05.055_b0165 article-title: Historical review of air-bearing spacecraft simulators publication-title: J. Guid. Control. Dyn. doi: 10.2514/2.5085 contributor: fullname: Schwartz – volume: 34 start-page: 351 year: 2006 ident: 10.1016/j.asr.2022.05.055_b0065 article-title: Design of satellite control system using optimal nonlinear theory publication-title: Mech. Based Des. Struct. Mach. doi: 10.1080/15397730601044853 contributor: fullname: De Souza – ident: 10.1016/j.asr.2022.05.055_b0015 – volume: 58 start-page: 1 year: 2006 ident: 10.1016/j.asr.2022.05.055_b0070 article-title: Representing attitude: Euler angles, unit quaternions, and rotation vectors publication-title: Matrix contributor: fullname: Diebel – volume: 4 start-page: 407 year: 2016 ident: 10.1016/j.asr.2022.05.055_b0110 article-title: Fuzzy Pid Controller for Nano-Satellite Attitude Control publication-title: J. Sci. Arts contributor: fullname: Mahdi – ident: 10.1016/j.asr.2022.05.055_b0155 – volume: 85 start-page: 106679 issue: 1–13 year: 2020 ident: 10.1016/j.asr.2022.05.055_b0085 article-title: Hardware-in-the-loop real-time validation of micro-satellite attitude control publication-title: Comput. Electr. Eng. doi: 10.1016/j.compeleceng.2020.106679 contributor: fullname: Gaber – start-page: 1372 year: 2019 ident: 10.1016/j.asr.2022.05.055_b0005 article-title: Intelligent Fuzzy PD+I Controller with Stabilizer for Nano Satellite Attitude Control System publication-title: J. Phys. Conf. Ser. contributor: fullname: Ahmed – start-page: 1 year: 2018 ident: 10.1016/j.asr.2022.05.055_b0030 article-title: Comparison of fuzzy and pid controllers for the attitude control of nanosatellites publication-title: Adv. Intell. Syst. Comput. contributor: fullname: Calvo – volume: 54 start-page: 1 issue: 5 year: 2017 ident: 10.1016/j.asr.2022.05.055_b0120 article-title: Lorentz-force-based fuzzy proportional-integral-derivative attitude control for earth-pointing satellites publication-title: J. Spacecr. Rockets doi: 10.2514/1.A33644 contributor: fullname: Mukherjee – volume: 64 start-page: 1466 year: 2019 ident: 10.1016/j.asr.2022.05.055_b0115 article-title: Small satellites for space science: A COSPAR scientific roadmap publication-title: Adv. Sp. Res. doi: 10.1016/j.asr.2019.07.035 contributor: fullname: Millan – volume: 21 start-page: 768 year: 2019 ident: 10.1016/j.asr.2022.05.055_b0130 article-title: Adaptive Fuzzy PID Control Strategy for Spacecraft Attitude Control publication-title: Int. J. Fuzzy Syst. doi: 10.1007/s40815-018-0576-2 contributor: fullname: Najafizadeh Sari – volume: 57 start-page: 137 year: 2016 ident: 10.1016/j.asr.2022.05.055_b0100 article-title: Spacecraft attitude control using neuro-fuzzy approximation of the optimal controllers publication-title: Adv. Sp. Res. doi: 10.1016/j.asr.2015.09.016 contributor: fullname: Kim – ident: 10.1016/j.asr.2022.05.055_b0080 doi: 10.1109/LARS/SBR/WRE.2018.00092 – volume: 115 start-page: 220 year: 1993 ident: 10.1016/j.asr.2022.05.055_b0215 article-title: Optimum settings for automatic controllers publication-title: J. Dyn. Syst. Meas. Control. Trans. ASME doi: 10.1115/1.2899060 contributor: fullname: Ziegler – volume: 19 year: 2012 ident: 10.1016/j.asr.2022.05.055_b0180 article-title: Application of the state-dependent riccati equation and kalman filter techniques to the design of a satellite control system publication-title: Shock Vib. contributor: fullname: Souza – ident: 10.1016/j.asr.2022.05.055_b0190 – volume: 19 start-page: 1444 year: 2017 ident: 10.1016/j.asr.2022.05.055_b0210 article-title: Interval Type-2 Fuzzy Sliding Mode Controller Based on Nonlinear Observer for a 3-DOF Helicopter with Uncertainties publication-title: Int. J. Fuzzy Syst. doi: 10.1007/s40815-016-0226-5 contributor: fullname: Zeghlache – volume: 10 start-page: 179 year: 2022 ident: 10.1016/j.asr.2022.05.055_b0170 article-title: Attitude Control of a Flexible Spacecraft via Fuzzy Optimal Variance Technique publication-title: Mathematics doi: 10.3390/math10020179 contributor: fullname: Sendi – volume: 36 start-page: 6613 year: 2009 ident: 10.1016/j.asr.2022.05.055_b0055 article-title: Attitude control of a satellite using fuzzy controllers publication-title: Expert Syst. Appl. doi: 10.1016/j.eswa.2008.08.053 contributor: fullname: Cheng – ident: 10.1016/j.asr.2022.05.055_b0075 – ident: 10.1016/j.asr.2022.05.055_b0175 doi: 10.1017/CBO9780511815652 – volume: 10 start-page: 976 year: 2022 ident: 10.1016/j.asr.2022.05.055_b0200 article-title: An Adaptive Neuro-Fuzzy Model for Attitude Estimation and Control of a 3 DOF System publication-title: Mathematics doi: 10.3390/math10060976 contributor: fullname: Wang – volume: 52 start-page: 1627 year: 2015 ident: 10.1016/j.asr.2022.05.055_b0195 article-title: Solely magnetic genetic/fuzzy-attitude-control algorithm for a CubeSat publication-title: J. Spacecr. Rockets doi: 10.2514/1.A33294 contributor: fullname: Walker – volume: 93 start-page: 1 year: 2021 ident: 10.1016/j.asr.2022.05.055_b0045 article-title: Adaptive fuzzy Jacobian control of spacecraft combined attitude and Sun tracking system publication-title: Aircr. Eng. Aerosp. Technol. doi: 10.1108/AEAT-02-2020-0038 contributor: fullname: Chak – ident: 10.1016/j.asr.2022.05.055_b0090 – volume: 69 start-page: 3204 year: 2022 ident: 10.1016/j.asr.2022.05.055_b0205 article-title: Magnetorquers-based satellite attitude control using interval type-II fuzzy terminal sliding mode control with time delay estimation publication-title: Adv. Sp. Res. doi: 10.1016/j.asr.2022.01.018 contributor: fullname: Yadegari – volume: 126 start-page: 546 year: 2016 ident: 10.1016/j.asr.2022.05.055_b0145 article-title: Verification of Spin Magnetic Attitude Control System using air-bearing-based attitude control simulator publication-title: Acta Astronaut. doi: 10.1016/j.actaastro.2016.03.028 contributor: fullname: Ousaloo – volume: 149 start-page: 107129 issue: 1–16 year: 2021 ident: 10.1016/j.asr.2022.05.055_b0125 article-title: Real-time implementation of a parameterized Model Predictive Control for Attitude Control Systems of rigid-flexible satellite publication-title: Mech. Syst. Signal Process. doi: 10.1016/j.ymssp.2020.107129 contributor: fullname: Murilo – volume: 354 start-page: 165 year: 2016 ident: 10.1016/j.asr.2022.05.055_b0035 article-title: A generalized type-2 fuzzy granular approach with applications to aerospace publication-title: Inf. Sci. (Ny) doi: 10.1016/j.ins.2016.03.001 contributor: fullname: Castillo – volume: 7 start-page: 111499 year: 2019 ident: 10.1016/j.asr.2022.05.055_b0020 article-title: Low-cost hardware-in-the-loop platform for embedded control strategies simulation publication-title: IEEE Access doi: 10.1109/ACCESS.2019.2934420 contributor: fullname: Bernardes – volume: 58 start-page: 102 year: 2016 ident: 10.1016/j.asr.2022.05.055_b0025 article-title: Fuzzy attitude control for a nanosatellite in low Earth orbit publication-title: Expert Syst. Appl. doi: 10.1016/j.eswa.2016.04.004 contributor: fullname: Calvo – volume: 1 start-page: 2581 year: 2021 ident: 10.1016/j.asr.2022.05.055_b0160 article-title: Challenge-Based Learning and Concurrent Engineering in Aerospace Engineering Education publication-title: INTED2021 Proc. doi: 10.21125/inted.2021.0551 contributor: fullname: Salgado Sánchez – volume: 67 start-page: 2081 year: 2012 ident: 10.1016/j.asr.2022.05.055_b0105 article-title: An anti-disturbance PD control scheme for attitude control and stabilization of flexible spacecrafts publication-title: Nonlinear Dyn. doi: 10.1007/s11071-011-0130-3 contributor: fullname: Liu |
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| Title | Experimental verification and comparison of fuzzy and PID controllers for attitude control of nanosatellites |
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