An analysis of the proposed Space Station Freedom Payload Pointing System (PPS) was performed to assess its dynamic payload pointing capability in the dynamic environment of the Space Station Freedom (SSF). In addition, the stability and control the the SSF was examined to verify the capability of its control devices to accommodate the impact of PPS operations. An analysis of the PPS ability to provide continuous, accurate pointing was performed and compared to the program requirements specified in the 1988 Program Definition and Requirement Document (PDRD). Results indicated that the PPS was not able to perform within the program requirements during the worst case scenario of a shuttle hard docking maneuver to the port side SSF docking ada...
Suitability of support and test equipment from the UARS Spacecraft Solar Stellar Pointing Platform (...
The long range objective of this task is to develop basic technology in the design, mechanization, a...
Gyroscope system for inertial experiment pointing and attitude control of manned spacecraf
The berthing maneuver is essential for the construction and assembly of Space Station Freedom (SSF) ...
Dynamic simulations of Space Station Freedom (SSF) configured with solar dynamic (SD) power modules ...
This paper describes the Annular Suspension and Pointing System (ASPS) being developed to support NA...
Technology assessment is performed for pointing systems that accommodate payloads of large mass and ...
Surveys of potential space station astrophysics payload requirements and existing point mount design...
The purpose of this paper is to provide final results of a pointing stability analysis for external ...
Viewgraphs on Space Station Freedom attitude determination and control system overview are presented...
The pointing and control of experiments during sortie missions are examined from the standpoint of a...
The Space Telescope pointing control system is designed to meet the fine pointing performance of 0.0...
This article addresses the role of man in operating on orbit a large pointing system such as the IPS...
The annular suspension and pointing system (ASPS) a payload auxiliary pointing device of the space s...
The Annular Suspension and Pointing System (ASPS) is a payload auxiliary pointing device of the Spac...
Suitability of support and test equipment from the UARS Spacecraft Solar Stellar Pointing Platform (...
The long range objective of this task is to develop basic technology in the design, mechanization, a...
Gyroscope system for inertial experiment pointing and attitude control of manned spacecraf
The berthing maneuver is essential for the construction and assembly of Space Station Freedom (SSF) ...
Dynamic simulations of Space Station Freedom (SSF) configured with solar dynamic (SD) power modules ...
This paper describes the Annular Suspension and Pointing System (ASPS) being developed to support NA...
Technology assessment is performed for pointing systems that accommodate payloads of large mass and ...
Surveys of potential space station astrophysics payload requirements and existing point mount design...
The purpose of this paper is to provide final results of a pointing stability analysis for external ...
Viewgraphs on Space Station Freedom attitude determination and control system overview are presented...
The pointing and control of experiments during sortie missions are examined from the standpoint of a...
The Space Telescope pointing control system is designed to meet the fine pointing performance of 0.0...
This article addresses the role of man in operating on orbit a large pointing system such as the IPS...
The annular suspension and pointing system (ASPS) a payload auxiliary pointing device of the space s...
The Annular Suspension and Pointing System (ASPS) is a payload auxiliary pointing device of the Spac...
Suitability of support and test equipment from the UARS Spacecraft Solar Stellar Pointing Platform (...
The long range objective of this task is to develop basic technology in the design, mechanization, a...
Gyroscope system for inertial experiment pointing and attitude control of manned spacecraf