Add to ORKGThe ship position and attitude measurement system that was installed aboard the tracking ship Vanguard is described. An overview of the entire system is given along with a description of how precise time and frequency is utilized. The instrumentation is broken down into its basic components. Particular emphasis is given to the inertial navigation system. Each navigation system used, a mariner star tracker, navigation satellite system, Loran C and OMEGA in conjunction with the inertial system is described. The accuracy of each system is compared along with their limitations
Investigating performance of various types of pure inertial and hybrid navigation system
The shuttle orbiter inertial measurement unit (IMU), located in the orbiter cabin, is used to supply...
Heretofor the evaluation of the Loran-A system has been carried out generally based on the astronomi...
The Global Positioning System (GPS) was developed to provide highly precise position, velocity, and ...
A satellite precision attitude control system was designed, based on the use of STARS as the princip...
Effects of time, frequency, and tracking station location errors on accuracy of trajectory analysi
Preflight operation and alignment of space stabilized inertial navigation system for vertical takeof...
The computer program for the real-time acquisition and tracking program uses a variety of filtering ...
Manual procedure for determining position in space from onboard optical measurements - celestial nav...
The use of satellite proper time as integration variable and space time correlation handling were ex...
Evaluation of precision distance measuring equipment for space shuttle landing navigatio
The purpose of this study was to evaluate potential uses of Global Positioning System (GPS) in space...
The application of GPS to spacecraft attitude determination is a new and growing field. Although the...
Simulation tests of attitude control system that uses star trackers and inertia wheel
This report presents the results of a preliminary investigation into the potential for applying NAVS...
Investigating performance of various types of pure inertial and hybrid navigation system
The shuttle orbiter inertial measurement unit (IMU), located in the orbiter cabin, is used to supply...
Heretofor the evaluation of the Loran-A system has been carried out generally based on the astronomi...
The Global Positioning System (GPS) was developed to provide highly precise position, velocity, and ...
A satellite precision attitude control system was designed, based on the use of STARS as the princip...
Effects of time, frequency, and tracking station location errors on accuracy of trajectory analysi
Preflight operation and alignment of space stabilized inertial navigation system for vertical takeof...
The computer program for the real-time acquisition and tracking program uses a variety of filtering ...
Manual procedure for determining position in space from onboard optical measurements - celestial nav...
The use of satellite proper time as integration variable and space time correlation handling were ex...
Evaluation of precision distance measuring equipment for space shuttle landing navigatio
The purpose of this study was to evaluate potential uses of Global Positioning System (GPS) in space...
The application of GPS to spacecraft attitude determination is a new and growing field. Although the...
Simulation tests of attitude control system that uses star trackers and inertia wheel
This report presents the results of a preliminary investigation into the potential for applying NAVS...
Investigating performance of various types of pure inertial and hybrid navigation system
The shuttle orbiter inertial measurement unit (IMU), located in the orbiter cabin, is used to supply...
Heretofor the evaluation of the Loran-A system has been carried out generally based on the astronomi...