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Chasqui I

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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.
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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.
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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;
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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
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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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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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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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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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Developed with assistance from the 8: 1009:MIP rendering of the subsystems of Chasqui I 335: 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 406: 386: 341: 334: 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 1062: 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. 666: 654: 629:Implementation of the laboratory 549:developed by students at Peru's 285: 249:. Please discuss further on the 228: 166: 64: 23: 1155:Project Official Site Chasqui 1 803:Image Acquisition System – SIMA 764:Power and Thermal Control – PCT 42:or discuss these issues on the 398: 1: 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 566:International Space Station 192:the claims made and adding 1192: 823:System Identification and 632:Development of the project 981:inertial reference system 772:Energy cycle of Chasqui I 534: 530: 501: 497: 473: 469: 439: 435: 352: 340: 294:This article needs to be 465:1 kilogram (2.2 lb) 952:Trajectory of Chasqui I 694:amateur radio frequency 1010: 958:differential equations 953: 915:wireless communication 910: 909:Block diagram of ESTER 901:Ground Station – ESTER 836: 812: 773: 745: 732: 75:relies excessively on 1008: 951: 908: 897:were also evaluated. 883:electromagnetic coils 835:Block diagram of SDCA 834: 811:Block diagram of SIMA 810: 771: 743: 730: 690:commercial components 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 580:—to take photos of 337: 1171:Student satellites 1011: 954: 911: 891:magnetic materials 871:angular velocities 837: 813: 774: 746: 733: 717:telecommunications 661:Chasqui I in space 601:General objectives 545:is a one-kilogram 506:Orbital parameters 177:possibly contains 1120:Nanosats Database 1103:. 18 August 2014. 993:method of order 4 626:Capacity building 538: 537: 333: 332: 325: 315: 314: 279: 278: 271: 242:with its subject. 222: 221: 214: 179:original research 160: 159: 152: 134: 57: 1183: 1130: 1129: 1127: 1126: 1111: 1105: 1104: 1091: 1085: 1084: 1082: 1081: 1067: 1051:List of CubeSats 825:Attitude Control 670: 658: 493: 491: 478:Start of mission 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Retrieved 1119: 1114:Kulu, Erik. 1109: 1098: 1089: 1078:. Retrieved 1074: 1065: 1012: 974: 955: 912: 852: 838: 814: 798: 790: 779: 775: 755: 747: 702: 679: 615: 611: 604: 588: 586: 576:and one for 563: 542: 541: 539: 357:Mission type 319: 303: 295: 265: 259:January 2010 256: 237: 208: 202:January 2010 199: 176: 146: 140:January 2010 137: 127: 120: 113: 106: 94: 74: 50: 43: 37: 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 1167:: 1118:. 1097:. 1073:. 1029:, 1025:, 1021:, 1017:, 972:. 865:, 597:. 584:. 90:. 48:. 1128:. 1083:. 492:) 326:) 320:( 308:) 304:( 298:. 272:) 266:( 261:) 257:( 253:. 215:) 209:( 204:) 200:( 182:. 153:) 147:( 142:) 138:( 128:· 121:· 114:· 107:· 84:. 55:) 51:(

Index

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National University of Engineering
COSPAR ID
1998-067ET
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SATCAT no.

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