| 1. Identity statement | |
| Reference Type | Journal Article |
| Site | plutao.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | J8LNKAN8RW/3C63NKH |
| Repository | dpi.inpe.br/plutao/2012/06.21.19.01 (restricted access) |
| Last Update | 2012:08.28.11.34.45 (UTC) administrator |
| Metadata Repository | dpi.inpe.br/plutao/2012/06.21.19.01.12 |
| Metadata Last Update | 2021:02.11.18.11.13 (UTC) administrator |
| ISSN | 0065-3438 |
| Label | lattes: 5801699053436537 1 SouzaAren:2012:DeSaCo |
| Citation Key | SouzaAren:2012:DeSaCo |
| Title | Design of Satellite Control Algorihtm Using the State Dependent Ricatti Equation and Kalman Filter  |
| Year | 2012 |
| Access Date | 2024, May 19 |
| Secondary Type | PRE PI |
| Number of Files | 1 |
| Size | 129 KiB |
| 2. Context | |
| Author | 1 Souza, Luiz Carlos Gadelha de 2 Arena, Victor M. R. |
| Resume Identifier | 1 8JMKD3MGP5W/3C9JHN3 |
| Group | 1 DMC-ETE-INPE-MCTI-GOV-BR |
| Affiliation | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Federal University of ABC, Santo André, São Paulo, Brazil |
| Author e-Mail Address | 1 gadelha@dem.inpe.br 2 varena@aluno.ufabc.edu.br |
| e-Mail Address | gadelha@dem.inpe.br |
| Journal | Advances in the Astronautical Sciences |
| Volume | I |
| Number | 2 |
| Pages | 235-243 |
| Secondary Mark | B3_ENGENHARIAS_III |
| History (UTC) | 2012-06-22 00:10:59 :: lattes -> secretaria.cpa@dir.inpe.br :: 2012 2012-08-28 11:34:46 :: secretaria.cpa@dir.inpe.br -> administrator :: 2012 2013-01-20 15:53:18 :: administrator -> banon :: 2012 2013-02-18 14:44:55 :: banon -> administrator :: 2012 2021-02-11 18:11:13 :: administrator -> marciana :: 2012 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Content Type | External Contribution |
| Keywords | Robust Control System State Dependent Ricatti Equation |
| Abstract | A properly attitude control algorithm design and test procedure can dramatically minimize space mission costs by reducing the number of errors that can be transmitted to the next phase of the project. Besides, when attitude control algorithm problems are discovered on-orbit the mission or at least part of it can be lost. One way to increase confidence in the control algorithm is its experimental validation through prototypes. The Space Mechanics and Control Division (DMC) of INPE is constructing a 3D simulator to supply the conditions for implementing and testing satellite hardware and software. The 3D simulator can accommodate various satellites components; like sensors, actuators, computers and its respective interface and electronic. Depending on the manoeuvre the 3D simulator plant can be highly non-linear and if its inertia parameters are not well determined the plant can also present some kind of uncertainty. As a result, controller designed by linear control technique can have its performance and robustness degraded. This paper presents the application of the State-Dependent Riccati Equation (SDRE) method in conjunction with Kalman filter to design and test a attitude control algorithm for a 3D satellite simulator. The control strategy is based on gas jets and reaction wheel torques to perform large angle manoeuvre in three axes. The simulator model allows investigating the dynamics and the control system taking into account effects of the plant non-linearities and system noise. Initially, a simple comparison between the LQR and SDRE controller is performed. Practical applications are presented to address problems like presence of noise in process and measurements and incomplete state information using Kalman filter technique. Simulation has shown the performance and robustness of the SDRE controller applied for angular velocity reduction associated with stringent pointing requirement. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Design of Satellite... |
| doc Directory Content | access |
| source Directory Content | there are no files |
| agreement Directory Content | there are no files |
| 4. Conditions of access and use | |
| Language | en |
| User Group | administrator banon lattes secretaria.cpa@dir.inpe.br |
| Reader Group | administrator secretaria.cpa@dir.inpe.br |
| Visibility | shown |
| Archiving Policy | denypublisher denyfinaldraft |
| Read Permission | deny from all and allow from 150.163 |
| Update Permission | not transferred |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/446AF4B |
| Citing Item List | sid.inpe.br/bibdigital/2021/02.11.18.06 1 |
| URL (untrusted data) | http://www.space-flight.org/docs/2012_winter/2012_winter.html |
| Dissemination | WEBSCI; PORTALCAPES; MGA; COMPENDEX. |
| Host Collection | dpi.inpe.br/plutao@80/2008/08.19.15.01 |
| 6. Notes | |
| Notes | Setores de Atividade: Atividades profissionais, científicas e técnicas. |
| Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi format isbn lineage mark mirrorrepository month nextedition orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject targetfile tertiarymark tertiarytype typeofwork versiontype |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |