Command and Data Handling Subsystem Design for the Ionospheric Observation Nanosatellite Formation (ION-F)

نویسندگان

  • John D. Jensen
  • Charles M. Swenson
چکیده

This paper describes the approach taken by the ION-F student team in designing a common Command and Data Handling (C&DH) subsystem for three different nanosatellites. It outlines the requirements of the satellites and reasons behind the decision to develop a custom board. The design is based upon industrial-grade components and centered on a Hitachi SuperH RISC Processor. The C&DH subsystem contains a 16 MB telemetry buffer, a digital and analog interface subsystem, and a DMA-oriented CMOS camera framebuffer. Students are fabricating these boards with the assistance of Space Dynamics Laboratory at Utah State University. This design will be flown by three different satellites, which are all part of a single formation-flying mission.

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Attitude Determination for Small Satellites with Modest Pointing Constraints

This monograph reports on the development of the attitude determination backbone of the Ionospheric Observation Nanosatellite Formation (ION-F). Three spacecraft with similarly modest pointing constraints comprise the ION-F constellation. Pointing requirements for the constellation are dictated by the formation flying mission objective and communication demands. To satisfy pointing requirements...

متن کامل

Design, Analysis, Fabrication, and Testing of a Nanosatellite Structure

The satellite industry is undergoing a transition toward " smallsat " engineering. Small satellites are becoming more attractive to customers as a method of decreasing cost. As the launch costs remain relatively constant, the industry is turning towards nano–technology, such as microelectromechanical systems, and distributed satellite systems to perform the same missions that once required supe...

متن کامل

Differential Flatness Method Based on Pre-set Guidance and Control Subsystem Design for a Surface to Surface Flying Vehicle (TECHNICAL NOTE)

The purpose of this paper is to design a guidance and control system and evaluate the performance of a sample surface‑to‑surface flying object based on preset guidance with a new prospective. In this study, the main presented idea is usage of unique property of governor differential equations in order to design and develop a controlled system. Thereupon a set of system output variables have bee...

متن کامل

Design and Development of Low Cost Command and Data Handling Subsystem Kit for Cubesat

Commercial CubeSat kit was introduced to shortened development process by providing standard hardware for CubeSat’s subsystems. However, project team still needs to do a lot of coordination for subsystems integration. Price of the kits is also expensive, especially when converted to Malaysian Ringgit. This project is aimed to design and develop a low cost Command and Data Handling (C&DH) subsys...

متن کامل

Model of Process Critique of Contemporary Residential Works Based on the components: "Mission, Objectives, Functional Needs and Concepts

The formation of a designer's personality and the acquisition of design skills are dependent on specific components and variables, such as observation and sampling, analysis and handling of samples, direct involvement and impregnation with the design problem. Architectural critique and analysis of the works of the past and successful and unsuccessful examples have always played a key role in ar...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2000