Author:
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9781563479113
Category : Space vehicles
Languages : en
Pages : 47
Book Description
Mass Properties Control for Space Systems
Author:
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9781563479113
Category : Space vehicles
Languages : en
Pages : 47
Book Description
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9781563479113
Category : Space vehicles
Languages : en
Pages : 47
Book Description
Space Systems. Mass Properties Control
Author: British Standards Institute Staff
Publisher:
ISBN: 9780580554780
Category :
Languages : en
Pages : 24
Book Description
Space technology, Spacecraft, Space vehicles, Mass, Weight (mass), Management, Project management
Publisher:
ISBN: 9780580554780
Category :
Languages : en
Pages : 24
Book Description
Space technology, Spacecraft, Space vehicles, Mass, Weight (mass), Management, Project management
Recommended Practice for Mass Properties Control for Satellites, Missiles, and Launch Vehicles
Author: American Institute of Aeronautics and Astronautics
Publisher: AIAA Standards
ISBN: 9781563473876
Category : Technology & Engineering
Languages : en
Pages : 0
Book Description
This recommended practice provides a methodology for mass properties control through the multiple phases of space hardware development. It defines the development stages and describes a control process which meets expectations in all sectors of the aerospace industry.
Publisher: AIAA Standards
ISBN: 9781563473876
Category : Technology & Engineering
Languages : en
Pages : 0
Book Description
This recommended practice provides a methodology for mass properties control through the multiple phases of space hardware development. It defines the development stages and describes a control process which meets expectations in all sectors of the aerospace industry.
System Characterization and Online Mass Property Identification of the SPHERES Formation Flight Testbed
Author: Dustin Scott Berkovitz
Publisher:
ISBN:
Category :
Languages : en
Pages : 155
Book Description
The National Aeronautics and Space Administration (NASA) and other entities in the aerospace industry have recently been considering distributed architectures for many space applications, such as space-based interferometry. Whether the craft in such a system are structurally connected or flown in tight formation, distribution allows for higher redundancy in case of failures as well as reducing the minimum payload footprint for launch. Designed to fly in precise formation, the SPHERES satellites rely on accurate system characteristics such as thruster strength and vehicle mass and inertia. The SPHERES testbed is described and the applications for formation flight are presented. Mass properties of the SPHERES satellites are examined because of their impact on control determination, with comparison between CAD model estimates and empirically determined values. The sensor and actuator suite, essential for closed-loop control, are also identified and characterized. A recursive least squares algorithm for determining mass properties in real time is explained and implemented both offline and online with results from test flights aboard NASA's KC-135 micro-gravity aircraft (Reduced Gravity Airplane, RGA).
Publisher:
ISBN:
Category :
Languages : en
Pages : 155
Book Description
The National Aeronautics and Space Administration (NASA) and other entities in the aerospace industry have recently been considering distributed architectures for many space applications, such as space-based interferometry. Whether the craft in such a system are structurally connected or flown in tight formation, distribution allows for higher redundancy in case of failures as well as reducing the minimum payload footprint for launch. Designed to fly in precise formation, the SPHERES satellites rely on accurate system characteristics such as thruster strength and vehicle mass and inertia. The SPHERES testbed is described and the applications for formation flight are presented. Mass properties of the SPHERES satellites are examined because of their impact on control determination, with comparison between CAD model estimates and empirically determined values. The sensor and actuator suite, essential for closed-loop control, are also identified and characterized. A recursive least squares algorithm for determining mass properties in real time is explained and implemented both offline and online with results from test flights aboard NASA's KC-135 micro-gravity aircraft (Reduced Gravity Airplane, RGA).
Technology for Large Space Systems
Author:
Publisher:
ISBN:
Category : Large space structures (Astronautics)
Languages : en
Pages : 280
Book Description
Publisher:
ISBN:
Category : Large space structures (Astronautics)
Languages : en
Pages : 280
Book Description
Apollo Program- Mass Properties Standard
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
Techniques for the Determination of Mass Properties of Earth-to-orbit Transportation Systems
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 112
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 112
Book Description
Mass Properties Control Requirements for STEP Mission 4
Author: Donald L. Jones
Publisher:
ISBN:
Category :
Languages : en
Pages : 11
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 11
Book Description
Mass Properties Analysis and Control of Advanced Space Structures Through Computerized Integration with Design and Structural Analysis
Author: John H. Nakai
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
Mass Properties Control of a Spin Stabilized Spacecraft with Restrictive Mission and Weight Constraints
Author: William Eric Lang
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description