Advances in Inertial Guidance Technology for Aerospace Systems
Author(s)
Braun, Robert D.
Putnam, Zachary R.
Steinfeldt, Bradley A.
Grant, Michael J. J.
Advisor(s)
Editor(s)
Collections
Supplementary to:
Permanent Link
Abstract
The origin, evolution, and outlook of guidance as a path and trajectory manager for
aerospace systems is addressed. A survey of theoretical developments in the field is
presented demonstrating the advances in guidance system functionality built upon
inertial navigation technology. Open-loop and closed-loop approaches for short-range
systems, long-range systems and entry systems are described for both civilian and
military applications. Over time, guidance system development has transitioned from
passive and open-loop systems to active, closed-loop systems. Significant advances in
onboard processing power have improved guidance system capabilities, shifting the
algorithmic computational burden to onboard systems and setting the stage for
autonomous aerospace systems. Seminal advances in aerospace guidance are described,
highlighting the advancements in guidance and resulting performance improvements in
aerospace systems.
Sponsor
Date
2013-08
Extent
Resource Type
Text
Resource Subtype
Paper
Rights Statement
Unless otherwise noted, all materials are protected under U.S. Copyright Law and all rights are reserved