DocumentCode
2593465
Title
Avionics systems for advanced launch vehicles
Author
Nelson, Kurt D.
Author_Institution
Gen. Dynamics, San Diego, CA, USA
fYear
1990
fDate
15-18 Oct 1990
Firstpage
430
Lastpage
435
Abstract
A brief description of the successful pre-planned product improvement program used for the integration of modern avionics into the Centaur upper stage system is used to illustrate the implementation of evolutionary changes to an existing launch system. This concept can be used to leverage industry technology to existing vehicles as well as new programs. A common module approach to standard avionics processing capabilities is developed to provide a technology evolution plan to benefit existing and future systems and reduce the total development risk. Topics discussed include multipath redundant avionics, adaptive guidance, navigation & control, electromechanical actuators, integrated GPS (Global Positioning System) with the inertial navigation system, and laser ordnance initiation systems
Keywords
adaptive systems; aerospace control; aerospace instrumentation; electric actuators; inertial navigation; radionavigation; satellite relay systems; Centaur upper stage; Global Positioning System; adaptive guidance; advanced launch vehicles; avionics; control; data acquisition; development risk; electromechanical actuators; inertial navigation; integrated GPS; laser ordnance initiation; multipath redundant avionics; navigation; redundancy; Adaptive control; Aerospace electronics; Control systems; Electrical equipment industry; Global Positioning System; Intelligent vehicles; Navigation; Optical control; Programmable control; Standards development;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
Conference_Location
Virginia Beach, VA
Type
conf
DOI
10.1109/DASC.1990.111327
Filename
111327
Link To Document