| 1. Identity statement | ||||
| Reference Type | Journal Article | |||
| Site | mtc-m21b.sid.inpe.br | |||
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S | |||
| Identifier | 8JMKD3MGP5W34M/3FH88JP | |||
| Repository | sid.inpe.br/mtc-m21b/2014/01.09.16.47 (restricted access) | |||
| Last Update | 2015:03.11.14.02.46 (UTC) administrator | |||
| Metadata Repository | sid.inpe.br/mtc-m21b/2014/01.09.16.47.41 | |||
| Metadata Last Update | 2021:02.11.18.12.15 (UTC) administrator | |||
| DOI | 10.1088/1742-6596/465/1/012007 | |||
| ISSN | 1742-6588 | |||
| Citation Key | Rocco:2013:AuCoOr | |||
| Title | Automatic correction of orbital elements using continuous thrust controlled in closed loop  | |||
| Year | 2013 | |||
| Access Date | 2024, May 16 | |||
| Type of Work | journal article | |||
| Secondary Type | PRE PI | |||
| Number of Files | 1 | |||
| Size | 824 KiB | |||
| 2. Context | ||||
| Author | Rocco, Evandro Marconi | |||
| Resume Identifier | 8JMKD3MGP5W/3C9JH37 | |||
| Group | DMC-ETE-INPE-MCTI-GOV-BR | |||
| Affiliation | Instituto Nacional de Pesquisas Espaciais (INPE) | |||
| Author e-Mail Address | evandro@dem.inpe.br | |||
| e-Mail Address | marcelo.pazos@inpe.br | |||
| Journal | Journal of Physics: Conference Series | |||
| Volume | 465 | |||
| Number | 1 | |||
| Pages | Article number 012007 | |||
| Secondary Mark | B2 B2 B3 B5 B5 C C C C | |||
| History (UTC) | 2014-01-09 16:47:41 :: marciana -> administrator :: 2021-02-11 18:12:15 :: administrator -> marcelo.pazos@inpe.br :: 2013 | |||
| 3. Content and structure | ||||
| Is the master or a copy? | is the master | |||
| Content Stage | completed | |||
| Transferable | 1 | |||
| Content Type | External Contribution | |||
| Version Type | publisher | |||
| Abstract | This work aims to study and simulate the control of a spacecraft trajectory in order to correct automatically and simultaneously the orbital elements that define the orbit: semi-major axis, eccentricity, periapse argument, inclination and right ascension of the ascending node. Thus, to perform the control of the trajectory was used a propulsion system able to apply thrust with adjustable magnitude and direction of application. In this study it was considered that the propulsion system is controlled in closed loop, so the adjustments of the magnitude and direction of thrust depends on the error generated by comparing a reference state (position and velocity) and a current state. The reference state is determined according to the final orbital parameters. The current state is estimated at each step of the simulation, therefore, the reference and current states must be determined and compared at each step in order to generate the error signal that is inserted into the trajectory control system. However, the control of the orbital parameters simultaneously can be characterized as a multi-objective problem with conflicting goals. The correction of the semi-major axis causes an eccentricity modification and vice-versa. One possibility to deal with this problem is to define when and where to make adjustments for each of the parameters. Thus, the automatic control seeks the best way to correct each parameter, adjusting each one sequentially. At the end of the process all orbital parameters are automatically adjusted and maintained due to the use of the closed loop control system. | |||
| Area | ETES | |||
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Automatic correction of... | |||
| doc Directory Content | access | |||
| source Directory Content | there are no files | |||
| agreement Directory Content |
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| 4. Conditions of access and use | ||||
| Language | en | |||
| User Group | marcelo.pazos@inpe.br marciana | |||
| Reader Group | administrator marcelo.pazos@inpe.br marciana | |||
| Visibility | shown | |||
| Archiving Policy | denypublisher denyfinaldraft12 | |||
| Read Permission | deny from all and allow from 150.163 | |||
| Update Permission | not transferred | |||
| 5. Allied materials | ||||
| Mirror Repository | iconet.com.br/banon/2006/11.26.21.31 | |||
| Next Higher Units | 8JMKD3MGPCW/446AF4B | |||
| Citing Item List | sid.inpe.br/bibdigital/2021/02.11.18.06 5 sid.inpe.br/mtc-m21/2012/07.13.14.45.41 3 | |||
| Dissemination | WEBSCI; PORTALCAPES; SCOPUS. | |||
| Host Collection | sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 | |||
| 6. Notes | ||||
| Notes | 16th Brazilian Colloquium on Orbital Dynamics; Serra Negra, Sao Paulo; Brazil; 26 November 2012 through 30 November 2012 | |||
| Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel format isbn keywords label lineage mark month nextedition orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject targetfile tertiarymark tertiarytype url | |||
| 7. Description control | ||||
| e-Mail (login) | marcelo.pazos@inpe.br | |||
| update | ||||