Incorporation of scientific instruments into deep space probes.
Deep space probe design with regard to incorporation of scientific instrument payload
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Deep space probe design with regard to incorporation of scientific instrument payload
The Deep Space Network (DSN) network configurations used to generate the navigation observables and the basic process of deep space spacecraft navigation, from data generation through flight path determination and correction are described. Special emphasis is placed on the DSN Systems which generate the navigation data: the DSN Tracking and VLBI Systems. In addition, auxiliary navigational support functions are described.
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Unmanned spacecraft systems design for deep space probes, examining flyby and orbiter missions, attitude stabilization, etc
Unmanned spacecraft systems design for deep space probes, examining flyby and orbiter missions, attitude stabilization, etc
One-half rate convolutional encoding with sequential decoding for deep space probe telemetry links with application to Pioneer missions
The microwave telecommunication links between the earth and deep space probes have long been used to conduct radio science experiments which take advantage of the phase coherency and stability of these links. These experiments measure changes in the phase delay of the signals to infer electrical, magnetic and gravitational properties of the solar system environment and beyond through which the spacecraft and radio signals pass. The precision oscillators, from which the phase of the microwave signals are derived, play a key role in the stability of these links and therefore the sensitivity of these measurements. These experiments have become a driving force behind recent and future improvements in the Deep Space Network and spacecraft oscillators and frequency and time distribution systems. Three such experiments which are key to these improvements are briefly discussed and relationship between their sensitivity and the signal phase stability is described. The first is the remote sensing of planetary atmospheres by occultation in which the radio signal passes through the atmosphere and is refracted causing the signal pathlength to change from which the pressure and the temperature of the atmosphere can be derived. The second experiment is determination of the opacity of planetary rings by passage of the radio signals through the rings. The third experiment is the research for very low frequency gravitational radiation. The fractional frequency variation of the signal is comparable to the spatial strain amplitude the system is capable of detecting. A summary of past results and future possibilities for these experiments are presented.
Lightweight deep space probe design for spin stabilization
Solar array as primary electrical power source of Pioneer deep space probes, comparing performance data with test and design data
Statistical probability and sampled data method for compressing data from deep space probes
Ionospheric electron content from Faraday rotation measurements of earth satellite and deep space probe
Determination of efficient data format and data system for lightweight deep space probe
A document discusses a technique for enabling the reception of spacecraft commands at received signal levels as much as three orders of magnitude below those of current deep space systems. Tone-based commanding deals with the reception of commands that are sent in the form of precise frequency offsets using an open-loop receiver. The key elements of this technique are an ultrastable oscillator and open-loop receiver onboard the spacecraft, both of which are part of the existing New Horizons (Pluto flyby) communications system design. This enables possible flight experimentation for tone-based commanding during the long cruise of the spacecraft to Pluto. In this technique, it is also necessary to accurately remove Doppler shift from the uplink signal presented to the spacecraft. A signal processor in the spacecraft performs a discrete Fourier transform on the received signal to determine the frequency of the received signal. Due to the long-term drift in the oscillators and orbit prediction model, the system is likely to be implemented differentially, where changes in the uplink frequency convey the command information.
Quantile system of data compression for space telemetry
Onboard equipment for space probe data acquisition and transmission
Quantile system of data compression for space telemetry, discussing operation, efficiency and advantages
Design of spacebore central data system for solar probes
Interference effects of radiation from plutonium dioxide fueled radioisotope thermoelectric generator