Navigating the grand tours
Grand tours navigation system consisting of deep space network radio and onboard TV for future TOPS /Thermoelectric Outer Planet Spacecraft/ applications
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Grand tours navigation system consisting of deep space network radio and onboard TV for future TOPS /Thermoelectric Outer Planet Spacecraft/ applications
Tabulating trajectory data for alternate Grand Tour missions from earth for period 1976 to 1980
Grand Tour mission design, discussing navigation, trajectory parameters, launch vehicles and satellite flybys
Grand Tour missions centralized data handling, describing computer aided telemetry system and self testing and repairing control computer
Grand tours are a class of methods for visualizing multivariate data, or any finite set of points in n-space. The idea is to create an animation of data projections by moving a 2-dimensional projection plane through n-space. The path of planes used in the animation is chosen so that it becomes dense, that is, it comes arbitrarily close to any plane. One of the original inspirations for the grand tour was the experience of trying to comprehend an abstract sculpture in a museum. One tends to walk around the sculpture, viewing it from many different angles. A useful class of grand tours is based on the idea of continuously interpolating an infinite sequence of randomly chosen planes. Visiting randomly (more precisely: uniformly) distributed planes guarantees denseness of the interpolating path. In computer implementations, 2-dimensional orthogonal projections are specified by two 1-dimensional projections which map to the horizontal and vertical screen dimensions, respectively. Hence, a grand tour is specified by a path of pairs of orthonormal projection vectors. This paper describes an interpolation scheme for smoothly connecting two pairs of orthonormal vectors, and thus for constructing interpolating grand tours. The scheme is optimal in the sense that connecting paths are geodesics in a natural Riemannian geometry.
High energy fast Grand Tour multiplanet flyby missions to outer planets omitting Jupiter, noting identical arrival date at Neptune
IR experiments planning for Outer Planets Grand Tour including investigations of planetary radiation balance and atmospheric composition and satellites composition and physical properties
Trajectory analysis of multiplanet Grand Tour mission to four large outer planets on single flight, discussing mission planning
Trajectory analysis of multiplanet Grand Tour mission to four large outer planets on single flight, discussing mission planning
Multiplanet gravity assist grand tours in outer solar system, discussing launch opportunities and mission effects on spacecraft design
Outer planet explorers design for Grand Tour mission, discussing launch parameters, flight paths, environmental hazards, communications, ground control, navigation and power generation
Multiple outer planets flyby opportunities during 1976-1980 Grand Tour missions launch period, presenting computer generated specific encounter dates and flyby distances
PCM TV photographic data communication for grand tour of outer planets, emphasizing adaptive information-preserving data compression system for optimal performance
The estimation of trajectory correction requirements for the Outer Planets Grand Tour (OPGT) missions poses a unique and many-faceted problem for the systems analyst. In this paper the navigation concept for the OPGT is developed and illustrated. The limiting accuracies and performance of the combined radio/onboard optical system are examined. The combined orbit determination system is characterized by its accuracy and by its system risks. Such considerations are included with the statistical combination of maneuver estimates to produce preliminary delta V estimates for the planned OPGT missions.
Trajectories for 1976 to 1980 Grand Tours
Radiation effects on components of science instruments used on outer planets Grand Tour mission
Spacecraft computer centered data systems with standby redundancy, automated flexibility and LSI devices for grand tour mission
Asteroids flyby approaches during Jupiter missions and Grand Tours, obtaining gravitational deflection of spacecraft trajectories and mass cost estimates