Micro-satellite Reconfigurable Attitude Control Laws with Reaction Wheels Desaturation and Fault Management

التفاصيل البيبلوغرافية
العنوان: Micro-satellite Reconfigurable Attitude Control Laws with Reaction Wheels Desaturation and Fault Management
المؤلفون: M. Poderico, G. Morani
المصدر: Aerotecnica Missili & Spazio. 101:17-32
بيانات النشر: Springer Science and Business Media LLC, 2021.
سنة النشر: 2021
مصطلحات موضوعية: Attitude control, Computer science, Control limits, Law, Redundancy (engineering), Torque, Pharmacology (medical), Actuator, Fault (power engineering), Reaction wheel, Fault management
الوصف: This paper proposes a new reconfigurable control strategy for the attitude control of a Low Earth Orbit (LEO) micro-satellite equipped with reaction control wheels and reaction control thrusters (used as a secondary actuation system). Control laws are combined with control allocation algorithms that enable the optimal allocation of control effort in case of reaction wheels saturation and/or faults as well as when control limits are reached (e.g. maximum torques provided by reaction wheels). This allows to effectively use the redundancy of the actuators set and guarantee robust stability and control of the satellite attitude. The effectiveness of the proposed strategy has been assessed through a numerical analysis that includes several simulation scenarios, where different initial conditions have been set and also the fault of a reaction wheel has been simulated. Simulations have shown the ability of the control architecture to effectively manage several control issues (i.e. maximum achievable torques, reaction wheel saturation and faults) through the allocation of control effort among all the available control effectors.
تدمد: 2524-6968
0365-7442
DOI: 10.1007/s42496-021-00102-5
URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_________::ad3f29791e02be545837eaa048713867
https://doi.org/10.1007/s42496-021-00102-5
Rights: CLOSED
رقم الانضمام: edsair.doi...........ad3f29791e02be545837eaa048713867
قاعدة البيانات: OpenAIRE
الوصف
تدمد:25246968
03657442
DOI:10.1007/s42496-021-00102-5