A Systems Engineering Approach to the Design of a Spacecraft Dynamics and Control Testbed - Tapa blanda

Roach, Neal R.; Roche, Wayne C.

 
9781249449300: A Systems Engineering Approach to the Design of a Spacecraft Dynamics and Control Testbed
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ISBN 10: 1249449308 ISBN 13: 9781249449300
Editorial: BiblioScholar, 2012

Sinopsis

A systems engineering team used an innovative process to develop a new frictionless air bearing satellite simulator, SIMSAT II, for AFIT. AFIT faculty provided the design team with initial requirements, including rotating 30 rpm for spin stabilization and a rapid slewing capability about the yaw axis of +/- 45 degrees in 15 seconds from a standing start to a standing stop. The design team developed the Project Vee process model to meet these requirements by combining key system engineering principles of the original Vee model with project management tenets. The Project Vee model decomposed the requirements to produce a complete system design, guided the procurement of components, and performed validation and verification of the system. The design effort resulted in a three-axis, tabletop spherical air bearing configuration. SIMSAT II incorporates the use of fans as an actuating device for rapid slewing capability, a rigid structure for greater stability, and the capability for longer experimental runs. A modular payload platform allows for numerous types of experiments to be conducted onboard the system. SIMSAT II provides AFIT with a new simulator for spacecraft dynamics and control, with both educational and research experimentation possibilities.

"Sinopsis" puede pertenecer a otra edición de este libro.

Reseña del editor

A systems engineering team used an innovative process to develop a new frictionless air bearing satellite simulator, SIMSAT II, for AFIT. AFIT faculty provided the design team with initial requirements, including rotating 30 rpm for spin stabilization and a rapid slewing capability about the yaw axis of +/- 45 degrees in 15 seconds from a standing start to a standing stop. The design team developed the Project Vee process model to meet these requirements by combining key system engineering principles of the original Vee model with project management tenets. The Project Vee model decomposed the requirements to produce a complete system design, guided the procurement of components, and performed validation and verification of the system. The design effort resulted in a three-axis, tabletop spherical air bearing configuration. SIMSAT II incorporates the use of fans as an actuating device for rapid slewing capability, a rigid structure for greater stability, and the capability for longer experimental runs. A modular payload platform allows for numerous types of experiments to be conducted onboard the system. SIMSAT II provides AFIT with a new simulator for spacecraft dynamics and control, with both educational and research experimentation possibilities.

"Sobre este título" puede pertenecer a otra edición de este libro.

Editorial
BiblioScholar
Año de publicación
2012
Idioma
Inglés
ISBN 10 
1249449308
ISBN 13 
9781249449300
Encuadernación
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Número de páginas
286
Contacto del fabricante
no disponible
Persona responsable
no disponible

Otras ediciones populares con el mismo título

9781025086439: A Systems Engineering Approach to the Design of a Spacecraft Dynamics and Control Testbed

Edición Destacada

ISBN 10:  1025086430 ISBN 13:  9781025086439
Editorial: Hutson Street Press, 2025
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