UNLIMITED FREE
ACCESS
TO THE WORLD'S BEST IDEAS

SUBMIT
Already a GlobalSpec user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your GlobalSpec Experience

Finish!
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

NASA-LLIS-1617

Lessons Learned – Fin Actuator System (FAS)/High Current Transients in Digital Circuits

active, Most Current
Organization: NASA
Publication Date: 2 June 2005
Status: active
Page Count: 3
scope:

Abstract:

The Pegasus actuator system was redesigned to accommodate the need for greater hinge torque. The decision to re-utilize, as much as possible, of the existing legacy actuator drive system is not necessarily a poor choice. However, one must understand that significantly increasing the performance requirements will stress all components in the (sub)system. Instantaneous currents associated with digital switching of power components can far exceed the steady-state values. When considering undertaking a significant redesign of a system or sub-system, extreme care must be taken to ensure that reutilization of existing components, i.e. motherboards, power supplies, cabling, etc., doesn't pose a greater risk than the initial cost and schedule impact of a complete (sub)system redesign.

Document History

NASA-LLIS-1617
June 2, 2005
Lessons Learned – Fin Actuator System (FAS)/High Current Transients in Digital Circuits
Abstract: The Pegasus actuator system was redesigned to accommodate the need for greater hinge torque. The decision to re-utilize, as much as possible, of the existing legacy actuator drive system...
Advertisement