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Application of MPC to Spacecraft Attitude Maneuver using RCS and/or RW

Takeya ASAKAWA, Takashi KIDA
<span title="">2013</span> <i title="Japan Society of Mechanical Engineers"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/yxipc2yq4zaxrdj7xroyood5pm" style="color: black;">Journal of Space Engineering</a> </i> &nbsp;
This paper applies model predictive control (MPC) to multi-input spacecraft attitude maneuver problems using reaction control systems (RCS) and reaction wheels (RW).  ...  For this purpose, we consider linear quadratic cost functions under the input constraints of nonlinear on-off control inputs for RCS and linear continuous inputs with saturation for RW.  ...  An RCS can produce large torque inputs compared with RW, so it is useful for large angle rotations or high-speed switching maneuvers of heavy spacecraft, although it takes only integer values.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1299/spacee.6.1">doi:10.1299/spacee.6.1</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/sycqiawqpvbydov4kmzg22e6qa">fatcat:sycqiawqpvbydov4kmzg22e6qa</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20181103191718/https://www.jstage.jst.go.jp/article/spacee/6/1/6_1/_pdf" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] <div class="menu fulltext-thumbnail"> <img src="https://blobs.fatcat.wiki/thumbnail/pdf/ee/40/ee406ee0abb84dd7088e880ae3fbfaefe2c35ff4.180px.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1299/spacee.6.1"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="external alternate icon"></i> Publisher / doi.org </button> </a>

A Novel Concept for Guidance and Control of Spacecraft Orbital Maneuvers

Matteo Dentis, Elisa Capello, Giorgio Guglieri
<span title="">2016</span> <i title="Hindawi Limited"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/75xpl4z7arculfjaok5ombj2ju" style="color: black;">International Journal of Aerospace Engineering</a> </i> &nbsp;
The purpose of this paper is the design of guidance and control algorithms for orbital space maneuvers.  ...  A combination of guidance and control algorithms for an orbital maneuver is proposed: (i) a suitably designed Zero-Effort-Miss/Zero-Effort-Velocity (ZEM/ZEV) algorithm is adopted for the guidance and (  ...  For the evaluation of the spacecraft attitude angular velocities and angles, the body reference frame is considered, the origin of which is the center of mass of the spacecraft (see Figure 3 ).  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1155/2016/7695257">doi:10.1155/2016/7695257</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/t6ndacxvtbcbfi75ojr3puw2bq">fatcat:t6ndacxvtbcbfi75ojr3puw2bq</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20190426152929/https://iris.polito.it/retrieve/handle/11583/2658327/136162/7695257.pdf" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] <div class="menu fulltext-thumbnail"> <img src="https://blobs.fatcat.wiki/thumbnail/pdf/d5/f7/d5f7f281f3953c804893c10a9bde40882dd91ebe.180px.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1155/2016/7695257"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="unlock alternate icon" style="background-color: #fb971f;"></i> hindawi.com </button> </a>

"Flyable" Guidance and Control Algorithms for Orbital Rendezvous Maneuver

Elisa CAPELLO, Fabrizio DABBENE, Giorgio GUGLIERI, Elisabetta PUNTA
<span title="">2018</span> <i title="The Society of Instrument and Control Engineers"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/ts2kn3kfmfcxhldnkhesf6bfcy" style="color: black;">SICE Journal of Control Measurement and System Integration</a> </i> &nbsp;
The aim of this paper is to provide an overview of some recent algorithms for guidance and control systems, and also their combined exploitation, which can provide significant enhancements.  ...  Rendezvous orbital maneuvers are planned operations which intend to make two spacecraft meet, while avoiding collisions.  ...  on a real application: (1) reduced frequency of the controller for fuel saving, (2) pulse width modulation of thrusters and (3) realistic actuator models.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.9746/jcmsi.11.14">doi:10.9746/jcmsi.11.14</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/7t57ufbisrh4dnm3l5a3ige5ue">fatcat:7t57ufbisrh4dnm3l5a3ige5ue</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20181102091043/https://www.jstage.jst.go.jp/article/jcmsi/11/1/11_14/_pdf" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] <div class="menu fulltext-thumbnail"> <img src="https://blobs.fatcat.wiki/thumbnail/pdf/b4/a0/b4a0e2e1d918c1393ff704cfe34e5549232172db.180px.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.9746/jcmsi.11.14"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="external alternate icon"></i> Publisher / doi.org </button> </a>

Precise Attitude Control Techniques: Performance Analysis From Classical to Variable Structure Control [chapter]

Elisa Capello, Matteo Dentis
<span title="2020-01-15">2020</span> <i title="IntechOpen"> Advances in Spacecraft Attitude Control </i> &nbsp;
Keywords: precise attitude control, continuous twisting controller, model predictive control, pointing stability, variable structure control 7 7 5 , with k 1 ¼  ...  Different control techniques are analyzed: (i) a tube-based robust model predictive control (MPC) and (ii) a variable gain continuous twisting (CT) sliding mode controller.  ...  Conclusions In the proposed research, small spacecraft attitude tracking with two advanced robust control laws has been developed: (i) a tube-based robust model predictive control and (ii) a continuous  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.5772/intechopen.90023">doi:10.5772/intechopen.90023</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/4hayjnyftffmbbql4clzpwiqoy">fatcat:4hayjnyftffmbbql4clzpwiqoy</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20200508004616/https://api.intechopen.com/chapter/pdf-download/70008.pdf" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] <div class="menu fulltext-thumbnail"> <img src="https://blobs.fatcat.wiki/thumbnail/pdf/7d/03/7d03175224b5e0c653efe5c9a39ba0937de4c5a8.180px.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.5772/intechopen.90023"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="unlock alternate icon" style="background-color: #fb971f;"></i> Publisher / doi.org </button> </a>

Critical GNC Aspects for ADR missions

João Branco, Pablo Colmenarejo, Pedro Serra, Pedro Lourenço, Thomas V. Peters, Marco Mammarella
<span title="2021-06-25">2021</span> <i title="Zenodo"> Zenodo </i> &nbsp;
In addition to outlining some of the main challenges and describing the state-of-the-art of GNC responses, it outlines consolidated methodologies for design, development, verification and validation to  ...  In the past decade, GMV has been, both as a participant and a reviewer, at the forefront of ESA's efforts in identifying and responding to criticalities in GNC technologies for future ADR and in-orbit  ...  The GUIBEAR project has demonstrated the combination of Model Predictive Control with bearings-only navigation for far-range rendezvous isfeasible from the point of view of the G&N.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.5281/zenodo.6410287">doi:10.5281/zenodo.6410287</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/qibkj3akg5hyvpbb7ndroacvmm">fatcat:qibkj3akg5hyvpbb7ndroacvmm</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20220521045528/https://zenodo.org/record/6410288/files/Branco%20et%20al_2021_Critical%20GNC%20Aspects%20for%20ADR%20missions.pdf" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] <div class="menu fulltext-thumbnail"> <img src="https://blobs.fatcat.wiki/thumbnail/pdf/93/92/9392dab03ffc04c7000d8350d7b5d837c8777940.180px.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.5281/zenodo.6410287"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="unlock alternate icon" style="background-color: #fb971f;"></i> zenodo.org </button> </a>

Estimation of a Spacecraft's Attitude Dynamics Parameters by Using Flight Data

Mark L. Psiaki
<span title="">2005</span> <i title="American Institute of Aeronautics and Astronautics (AIAA)"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/yekwqy6srncl5bew6tynp7vjsq" style="color: black;">Journal of Guidance Control and Dynamics</a> </i> &nbsp;
The first is about 6 h long and starts at 15:19 UT on 1 July 2001. It includes 10 large-angle slew maneuvers that are controlled by the reaction wheels.  ...  Introduction HE goal of this research is to develop improved Euler attitude dynamics models for spacecraft by using flight data to estimate model parameters.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.2514/1.7362">doi:10.2514/1.7362</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/kt4tk4g72bhtvicu3c62vnrq7u">fatcat:kt4tk4g72bhtvicu3c62vnrq7u</a> </span>
<a target="_blank" rel="noopener" href="https://archive.org/details/sim_journal-of-guidance-control-and-dynamics_july-august-2005_28_4/page/594" title="read fulltext microfilm" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Archive [Microfilm] <div class="menu fulltext-thumbnail"> <img src="https://archive.org/serve/sim_journal-of-guidance-control-and-dynamics_july-august-2005_28_4/__ia_thumb.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.2514/1.7362"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="external alternate icon"></i> Publisher / doi.org </button> </a>

Conference Digest

<span title="">2020</span> <i title="IEEE"> 2020 IEEE Aerospace Conference </i> &nbsp;
of measuring Martian air temperature, wind speed, atmospheric pressure, and local magnetic fields.  ...  The Auxiliary Payload Sensor Suite (APSS), a collection of environmental sensors carried by the Interior exploration using Seismic Investigations, Geodesy, and Heat Transport (InSight) lander, is capable  ...  Simulation results of the developed nonlinear relative motion model show the effect of differential J_2 and drag captured by the equations for a LEO leader-follower formation with large intersatellite  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1109/aero47225.2020.9172613">doi:10.1109/aero47225.2020.9172613</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/ioqf5ijrx5gvffu3ls34aa2nsq">fatcat:ioqf5ijrx5gvffu3ls34aa2nsq</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20200822062844/https://ieeexplore.ieee.org/ielx7/9161765/9172248/09172613.pdf?tp=&amp;arnumber=9172613&amp;isnumber=9172248&amp;ref=" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1109/aero47225.2020.9172613"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="external alternate icon"></i> ieee.com </button> </a>

The Lynx Mission Concept Study Interim Report [article]

The Lynx Team
<span title="2018-09-25">2018</span> <i > arXiv </i> &nbsp; <span class="release-stage" >pre-print</span>
angular resolution with high throughput; 16 times larger field of view (FOV) for sub-arcsecond imaging; and 10-20 times higher spectral resolution for both point-like and extended sources.  ...  Lynx will see the dawn of black holes, reveal what drives galaxy formation and evolution, and unveil the energetic side of stellar evolution and stellar ecosystems.  ...  Data Handling (C&DH) System .06.07.01.01 5 Flight Computer .06.07.01.02 5 Solid State Recorder .06.07.01.03 5 Data Acquisition Unit .06.07.01.04 5 RCS Controller .06.07.01.05 5 RW Controller  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener" href="https://arxiv.org/abs/1809.09642v1">arXiv:1809.09642v1</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/f65tmsqtdvgfhbv5k4bj4fvf3m">fatcat:f65tmsqtdvgfhbv5k4bj4fvf3m</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20200930191030/https://arxiv.org/ftp/arxiv/papers/1809/1809.09642.pdf" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] <div class="menu fulltext-thumbnail"> <img src="https://blobs.fatcat.wiki/thumbnail/pdf/e3/5c/e35c99c1198efd295b056bcadf51a40afaf1d01f.180px.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener" href="https://arxiv.org/abs/1809.09642v1" title="arxiv.org access"> <button class="ui compact blue labeled icon button serp-button"> <i class="file alternate outline icon"></i> arxiv.org </button> </a>

High angle of attack aerodynamics

J.L. Stollery
<span title="">1992</span> <i title="Elsevier BV"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/ga5nrg2wtrbuzbwc6phgx4qztq" style="color: black;">Journal of Atmospheric and Terrestrial Physics</a> </i> &nbsp;
Hendriks in preparing the computer program for the reduction of the data is greatly appreciated. The assistance of Messrs. E.W. de Keizer, N.J. Lam and G.A.F.  ...  Bakker and T.P.M. 11endriks for their valuable contribution tomany discussions concerning the subject matter; also the expertness of Mr.  ...  Propulsion units for entry attitude control and orbital maneuvering have been incorporated in pods located in the aft body fairings.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1016/0021-9169(92)90172-h">doi:10.1016/0021-9169(92)90172-h</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/zku4imc4urdunb2wpc62vkpnmq">fatcat:zku4imc4urdunb2wpc62vkpnmq</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20170612061728/http://www.dtic.mil/get-tr-doc/pdf?AD=ADA067323" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1016/0021-9169(92)90172-h"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="external alternate icon"></i> elsevier.com </button> </a>

High Angle-of-Attack Aerodynamics

G. Erickson
<span title="1995-01-01">1995</span> <i title="Annual Reviews"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/2vgtdypqgzfnfmjizwftzs7e54" style="color: black;">Annual Review of Fluid Mechanics</a> </i> &nbsp;
Hendriks in preparing the computer program for the reduction of the data is greatly appreciated. The assistance of Messrs. E.W. de Keizer, N.J. Lam and G.A.F.  ...  Bakker and T.P.M. 11endriks for their valuable contribution tomany discussions concerning the subject matter; also the expertness of Mr.  ...  Propulsion units for entry attitude control and orbital maneuvering have been incorporated in pods located in the aft body fairings.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1146/annurev.fluid.27.1.45">doi:10.1146/annurev.fluid.27.1.45</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/fic5axsegnafbci3sbxlagjrky">fatcat:fic5axsegnafbci3sbxlagjrky</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20170612061728/http://www.dtic.mil/get-tr-doc/pdf?AD=ADA067323" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1146/annurev.fluid.27.1.45"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="external alternate icon"></i> Publisher / doi.org </button> </a>

High Angle-of-Attack Aerodynamics

G E Erickson
<span title="">1995</span> <i title="Annual Reviews"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/2vgtdypqgzfnfmjizwftzs7e54" style="color: black;">Annual Review of Fluid Mechanics</a> </i> &nbsp;
Hendriks in preparing the computer program for the reduction of the data is greatly appreciated. The assistance of Messrs. E.W. de Keizer, N.J. Lam and G.A.F.  ...  Bakker and T.P.M. 11endriks for their valuable contribution tomany discussions concerning the subject matter; also the expertness of Mr.  ...  Propulsion units for entry attitude control and orbital maneuvering have been incorporated in pods located in the aft body fairings.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1146/annurev.fl.27.010195.000401">doi:10.1146/annurev.fl.27.010195.000401</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/uzczhsvgs5evho5vak6q2hzmea">fatcat:uzczhsvgs5evho5vak6q2hzmea</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20170612061728/http://www.dtic.mil/get-tr-doc/pdf?AD=ADA067323" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1146/annurev.fl.27.010195.000401"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="external alternate icon"></i> Publisher / doi.org </button> </a>

Formulation of Torque-Optimal Guidance Trajectories for a CubeSat with Degraded Reaction Wheels

Siddharth Kedare, Steve Ulrich
<span title="">2016</span> <i title="American Institute of Aeronautics and Astronautics"> AIAA Guidance, Navigation, and Control Conference </i> &nbsp; <span class="release-stage">unpublished</span>
Results indicate that this torque-optimal guidance algorithm demonstrates substantial improvements in performance and pointing accuracy over an Eigenaxis controller for similar maneuvers, with low to moderate  ...  The mission life of nano-satellites may be limited by the attitude actuators, and it is therefore beneficial to reduce torque and angular momentum usage during reorientation maneuvers.  ...  Rao and his team for their insights into the internal workings and development of GPOPS. They also thank Dr.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.2514/6.2016-0088">doi:10.2514/6.2016-0088</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/5bzwp3n2qnbtzeenpsy72bvgz4">fatcat:5bzwp3n2qnbtzeenpsy72bvgz4</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20160616054323/http://carleton.ca:80/spacecraft/wp-content/uploads/AIAA-2016-0088.pdf" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] <div class="menu fulltext-thumbnail"> <img src="https://blobs.fatcat.wiki/thumbnail/pdf/9a/16/9a161a47dfdaffa3b74870f48f4e5946f7988e38.180px.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.2514/6.2016-0088"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="external alternate icon"></i> Publisher / doi.org </button> </a>

NONLINEAR APPROACHES TO ATTITUDE CONTROL USING MAGNETIC AND MECHANICAL ACTUATION Coordinatore Dottorato Relatore

Encarnación Castillo, Nicolò Cavina, Fabrizio Giulietti
<span class="release-stage">unpublished</span>
Emanuele de Angelis for introducing me in the attitude control field, his support during the initial part of the PhD track was really helpful, and to Prof. Giulio Avanzini for his useful advises.  ...  In this framework, the aim of this thesis is to develop novel control approaches for three-axis stabilisation of nanosatellites equipped with magnetorquers and reaction wheels, to improve the performance  ...  Although recent studies show a limited need for the development of new, or improvement of existing, analytical (modelling and simulation) tools for ACS, the performance of large-angle spacecraft attitude  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/c2skshrdcrh5tluxjdy6ggejgm">fatcat:c2skshrdcrh5tluxjdy6ggejgm</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20180412161046/http://amsdottorato.unibo.it/8090/1/Thesis_Serrano_Castillo.pdf" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] <div class="menu fulltext-thumbnail"> <img src="https://blobs.fatcat.wiki/thumbnail/pdf/2f/d9/2fd9b4f73ddf7da38814603469fdeed15ff1c02b.180px.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a>

A study of flexible space structures : dynamics and control

Anant Kiran Singh Grewal
<span title="">1994</span>
It is applicable to a large class of present and future spacecraft, and readily amenable to simulation of closed loop systems as well as control system synthesis.  ...  of the Jacobian matrices by finite differences; (f) ability to include a dynamic compensator model which allows for the simulation of the closed loop system consisting of a nonlinear plant and a linear  ...  management system for large angle maneuvers of rigid spacecraft using the LQR pole placement method 14 in conjunction with gain scheduling.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.14288/1.0080900">doi:10.14288/1.0080900</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/gr52ju6s5fcmzbqhwgta6ew6dm">fatcat:gr52ju6s5fcmzbqhwgta6ew6dm</a> </span>
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Recent advances in mechatronics

Okyay Kaynak
<span title="">1996</span> <i title="Elsevier BV"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/ncwahgzkgbfljbalytxadcov3u" style="color: black;">Robotics and Autonomous Systems</a> </i> &nbsp;
Typesetting: Camera-ready by Contributors SPIN 10717447 543210 (Robotics Society of Japan) and SICE (Society of Instr. and Control Engineers of Japan).  ...  The publisher makes no representation, express or implied, with regard to the accuracy of the information contained in this book and cannot accept any legal responsibility or liability for any errors or  ...  Tonegawa for his help with the experiments.  ... 
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