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Specific objectives of the project were to (1) establish contact and support other universities and institutions involved in such projects; (2) deepen the knowledge in emerging information and communications technologies; (3) lead projects within Latin
America; and (4) demonstrate and validate new
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The Power subsystem is responsible for receiving, processing, storing, and distributing power to other subsystems in the satellite. The objective of this subsystem is to ensure the necessary supply of electricity.
889:. The magnetorquers are especially important for the stabilization of the nanosatellite once it leaves the deployer. The inclusion of the permanent magnet creates a system of active-passive control. The use of
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The mechanical structure (EMEC) module was responsible for reviewing the state of field, comparing existing nanosatellite designs, and manufacturing the satellite based on the standard CubeSat format.
711:, surveillance of borders and territorial sea, and the prediction and mitigation of natural disasters. UNI, with its project Chasqui I, are taking steps in the process of addressing problems such as
791:
These subsystems also manage and monitor the state of the satellite, such as temperature, voltage and current. Both subsystems, including the heaters, were designed and built at UNI.
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maintains a pointing accuracy of 3° for taking pictures of Peru and, if technically possible, having a wide coverage of South
America through maneuvers of 30° roll and 30° pitch;
819:. Digital information is collected by the CCIM and then sent to the ground station (ESTER). Additionally, the module is responsible for processing digital images obtained.
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The SDCA enables
Chasqui I to determine its attitude, calculate the correction required to achieve the desired orientation, and execute the necessary maneuvers using the
703:
Peru has large geographical diversity, which makes it very difficult to constantly monitor the situation of natural and man-made events, such as permanent snow melting,
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subsystem is responsible for maintaining the proper temperature of the satellite components. The most critical task of this subsystem is to maintain the
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This subsystem maintains the nanosatellite's stabilization and orientation, adjusting the orientation when necessary. Specifically, the module
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stabilizes the nanosatellite after leaving the deployer through reduction (within 0.1rad / s) and control of angular velocities;
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that seeks to distinguish between fertile land and uncultivated areas. As a student project, Chasqui I was constructed using
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maintains a less demanding pointing accuracy (e.g. 20°) to enable data exchange between the satellite and ground station.
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This subsystem is responsible for providing a means of communication between the satellite and the ground station.
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nanosatellites. Plans for
Chasqui I included taking pictures of the Earth, with transmission to a ground station.
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This subsystem obtains photographs of the Earth using two cameras: one in the visible and the other in the
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917:(radio) needed to communicate with the Chasqui I (and any other satellite). Its main functions are:
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called the on-board computer (OBC), which fulfills the computing functions of all other subsystems.
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that allows for remote monitoring of the satellite, as well as satellites of other universities.
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This subsystem manages and monitors information from all subsystems of
Chasqui I. It contains a
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as sensors for determining attitude was also evaluated. The attitude control system uses
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Please help update this article to reflect recent events or newly available information.
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It may require cleanup to comply with
Knowledge (XXG)'s content policies, particularly
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This module aims to simulate the trajectory of
Chasqui I, which is calculated solving
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This module was responsible for the assembly of all the satellite components such as
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This simulation is accomplished by taking into consideration the following phases:
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on August 18, 2014. The concept satellite was equipped with two cameras—one for
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Most of UNI's objectives in satellite technology were completed through the
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Follow-up: radio for or hear the beacon or satellite for its position
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Obtain nonlinear equations of motion by considering the Earth as an
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196:. Statements consisting only of original research should be removed.
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Center for
Information & Communication Technologies (CTIC-UNI).
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Solve the equations of motion (energy remaining constant) using a
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1095:"Photos: Cosmonauts Take Spacewalk to Launch Peruvian Satellite"
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and permanent magnets as actuators, forming what are known as
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Simulation of displacements in the satellite's internal frame
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This ground-based subsystem consists of the facilities and
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Carry out trajectory simulations
Chasqui I using MATLAB
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within their operating limits of 0 °C–20 °C.
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A major contributor to this article appears to have a
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Home of the public university located in Lima Peru.
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752:Central Control and Information Management – CCIM
557:technology. Developed with assistance from the
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1009:MIP rendering of the subsystems of Chasqui I
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939:, reset the system, or take and send photos
53:Learn how and when to remove these messages
731:Outline of the project development modules
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323:Learn how and when to remove this message
269:Learn how and when to remove this message
212:Learn how and when to remove this message
150:Learn how and when to remove this message
1157:All information relating to the project.
935:Commando: order to extend the satellite
680:Chasqui I is a student research project
564:The nanosatellite was launched from the
16:Nanosatellite, first to be hand-deployed
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616:The stated goals of the project were:
587:The name of the project refers to the
86:Please improve this article by adding
7:
1001:Module Integration and Testing – MIP
1143:National University of Engineering
593:, who served as messengers in the
559:Russian Southwest State University
551:National University of Engineering
369:National University of Engineering
14:
34:This article has multiple issues.
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629:Implementation of the laboratory
549:developed by students at Peru's
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249:. Please discuss further on the
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1155:Project Official Site Chasqui 1
803:Image Acquisition System – SIMA
764:Power and Thermal Control – PCT
42:or discuss these issues on the
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859:attitude determination system
620:Design of the project profile
88:secondary or tertiary sources
795:Communication System – SICOM
736:Mechanical Structure – EMEC
705:deforestation of the Amazon
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192:the claims made and adding
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823:System Identification and
632:Development of the project
981:inertial reference system
772:Energy cycle of Chasqui I
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909:Block diagram of ESTER
901:Ground Station – ESTER
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75:relies excessively on
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511:Reference system
444:Spacecraft properties
247:neutral point of view
964:using two programs:
944:System Orbits – SORS
1075:Gunter's Space Page
985:Newton's second law
924:Telemetry: request
895:magnetic hysteresis
635:Testing integration
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506:Orbital parameters
177:possibly contains
1120:Nanosats Database
1103:. 18 August 2014.
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626:Capacity building
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1123:. Retrieved
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1114:Kulu, Erik.
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1078:. Retrieved
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357:Mission type
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259:January 2010
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140:January 2010
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36:Please help
33:
1116:"Chasqui-I"
1071:"Chasqui 1"
991:Runge-Kutta
932:calculation
867:Sun sensors
686:CMOS camera
595:Inca Empire
483:Launch date
462:Launch mass
99:"Chasqui I"
1165:Categories
1149:CTIC – UNI
1125:2024-06-14
1080:2024-06-14
1057:References
879:gyroscopes
692:. It uses
638:Guidelines
515:Geocentric
490:2014-08-18
382:1998-067ET
360:Scientific
306:April 2022
186:improve it
110:newspapers
77:references
39:improve it
1100:Space.com
1023:batteries
855:actuators
786:batteries
758:processor
641:Operation
570:spacewalk
568:during a
543:Chasqui I
525:Low Earth
376:COSPAR ID
347:Chasqui I
336:Chasqui I
251:talk page
190:verifying
45:talk page
1176:CubeSats
1045:See also
1027:antennas
962:parallel
873:. Using
578:infrared
423:.chasqui
365:Operator
1031:sensors
1019:cameras
937:antenna
719:areas.
646:Project
623:Funding
607:CubeSat
590:chasqui
555:CubeSat
488: (
456:CubeSat
416:Website
397:SATCAT
296:updated
184:Please
124:scholar
1033:, and
970:MATLAB
966:DelPhi
857:. The
827:– SDCA
521:Regime
126:
119:
112:
105:
97:
930:orbit
861:uses
582:Earth
404:40117
131:JSTOR
117:books
968:and
893:and
877:and
780:The
715:and
427:.edu
425:.uni
103:news
875:GPS
454:1U
450:Bus
429:.pe
421:www
399:no.
188:by
79:to
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