Abstract:
It is noted that with the development of the International Space Station Freedom, people will permanently live in space and require routine access and an assured crew ret...Show MoreMetadata
Abstract:
It is noted that with the development of the International Space Station Freedom, people will permanently live in space and require routine access and an assured crew return capability in case of emergencies in space. The extended duration in space requires a manned return vehicle that is less demanding on the crew and provides an autonomous deorbit, entry, and autoland capability. The authors discuss an autoland capability with an integrated differential GPS/INS that provides the required position and velocity accuracies without the need for tactical aircraft navigation (TACAN) and microwave landing system (MLS) navigation aides. Simulation results are used to demonstrate the feasibility of autoland using differential GPS aided with a high-precision altimeter. This concept applies to several manned space applications, such as Assured Crew Return Vehicle (ACRV), Assured Shuttle Availability (ASA), Advanced Manned Launch System (AMLS), and National Aerospace Plane (NASP), and to unmanned return vehicles such as the Propulsion Avionics Module (P/AM).<>
Published in: IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences
Date of Conference: 20-20 March 1990
Date Added to IEEE Xplore: 06 August 2002
References is not available for this document.
Select All
1.
T. Gust, Space Shuttle Autoland Design, August 1982.
2.
P.K. Enge, "Differential Operation of the Global Positioning System", IEEE Communications Magazine, July 1988.
3.
G. M. Ware, B. Spencer and J. R. Micol, Aerodynamic Characteristics of Proposed Assured Crew Return Capability (ACRC) Configurations, July 1989.
4.
M. Dzwonczyk and H. Stone, A Fault-Tolerant Avionics Suites for an Entry Research Vehicle, October 1988.
5.
F. G. Edwards and P. Y. N. Loomis, "Civil Helicopter Flight Operations using Differential GPS", Proceedings of the Autonomous All-Weather Navigation and Landing Workshop, 1986-January-27.
6.
C. I. Cruz and G. M. Ware, Aerodynamic Characteristics of a Proposed Personnel Launch System (PLS) Lifting Body Configuration at MACH Numbers from 0.05 to 20.3, August 1989.
