The computer program for the real-time acquisition and tracking program uses a variety of filtering algorithms including an extended Kalman filter to derive real-time orbit determination (position-velocity state vectors) from shipboard tracking and navigation data. Results from Apollo missions are given to show that orbital parameters can be estimated quickly and accurately using these methods
Precision attitude determination for recent and planned space missions typically includes quaternion...
Orbit of a spacecraft in three dimensional Inertial Reference Frame is in general represe...
A program installed in the ATSOCC on-line computer operates with attitude sensor data to produce a s...
Global Navigation Satellite System (GNSS) sensors on-board the space crafts are providing orbit dete...
Computer program for determining attitude of orbiting vehicle using Kalman filte
Leading up to the Apollo missions the Extended Kalman Filter, a modified version of the Kalman Filte...
As part of the Deep Space Network (DSN) advanced technology program an effort is underway to design ...
Doppler observable modeling and range difference technique for Apollo real time orbit determination ...
"July, 1982."Bibliography: p. 118-120.National Aeronautics and Space Administration and Langely Rese...
The literature since Apollo contains exhaustive material on attitude filtering, usually treating the...
textThis work documents the development of a real-time interplanetary orbit determination monitorin...
The Precision State and Filter Weighting Matrix Extrapolation Routine is described which provides th...
A navigation system for the entry phase of a Space Shuttle mission which is an aided-inertial system...
Statistical filter theory is employed to develop a method for determining the best possible estimate...
Kalman filter was pioneered by Rudolf Emil Kalman in 1960, originally designed and developed to solv...
Precision attitude determination for recent and planned space missions typically includes quaternion...
Orbit of a spacecraft in three dimensional Inertial Reference Frame is in general represe...
A program installed in the ATSOCC on-line computer operates with attitude sensor data to produce a s...
Global Navigation Satellite System (GNSS) sensors on-board the space crafts are providing orbit dete...
Computer program for determining attitude of orbiting vehicle using Kalman filte
Leading up to the Apollo missions the Extended Kalman Filter, a modified version of the Kalman Filte...
As part of the Deep Space Network (DSN) advanced technology program an effort is underway to design ...
Doppler observable modeling and range difference technique for Apollo real time orbit determination ...
"July, 1982."Bibliography: p. 118-120.National Aeronautics and Space Administration and Langely Rese...
The literature since Apollo contains exhaustive material on attitude filtering, usually treating the...
textThis work documents the development of a real-time interplanetary orbit determination monitorin...
The Precision State and Filter Weighting Matrix Extrapolation Routine is described which provides th...
A navigation system for the entry phase of a Space Shuttle mission which is an aided-inertial system...
Statistical filter theory is employed to develop a method for determining the best possible estimate...
Kalman filter was pioneered by Rudolf Emil Kalman in 1960, originally designed and developed to solv...
Precision attitude determination for recent and planned space missions typically includes quaternion...
Orbit of a spacecraft in three dimensional Inertial Reference Frame is in general represe...
A program installed in the ATSOCC on-line computer operates with attitude sensor data to produce a s...