lpetrich
Science Advisor
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Some pages on spacecraft navigation:
The Navigators: How We Fly Spacecraft Around the Solar System - Universe Today
How do space probes navigate large distances with such accuracy and how do the mission controllers know when they've reached their target? - Scientific American
Basics of Space Flight Section II. Space Flight Projects
Spacecraft Navigation
There are several sorts of data that spacecraft navigators use.
For doing the calculations, they typically do numerical integration, though analytic approximations are often good starting points. Approximations like the Newtonian two-body problem. For going from the Earth to Mars, one starts with geocentric calculations, then switches to heliocentric calculations for most of the trip, then switches to areocentric calculations at Mars.
They have to take into account not only celestial bodies' gravity, but also the pressure of sunlight and the solar wind. But they have gotten very good at that, and they also maintain very precise ephemerides, tables of the celestial bodies' positions. One can use spacecraft navigation data as inputs for those also.
The Navigators: How We Fly Spacecraft Around the Solar System - Universe Today
How do space probes navigate large distances with such accuracy and how do the mission controllers know when they've reached their target? - Scientific American
Basics of Space Flight Section II. Space Flight Projects
Spacecraft Navigation
There are several sorts of data that spacecraft navigators use.
- Pictures of the spacecraft . That's mainly useful in low Earth orbit. It gives the spacecraft 's direction relative to the stars from the observation site.
- Radio ranging. A round trip of a signal gives the spacecraft 's distance.
- Radio range rate. Doppler shift of the signal frequency gives the spacecraft 's radial velocity.
- Radio ranging with receivers in different positions, like on different continents. The relative arrival times and radial velocities can be combined to find the spacecraft 's direction.
- Optical navigation. The spacecraft takes an overexposed picture of a nearby celestial body, the overexposure being for seeing stars in nearby directions. This gives the body's direction, and if the body was resolved, its distance.
For doing the calculations, they typically do numerical integration, though analytic approximations are often good starting points. Approximations like the Newtonian two-body problem. For going from the Earth to Mars, one starts with geocentric calculations, then switches to heliocentric calculations for most of the trip, then switches to areocentric calculations at Mars.
They have to take into account not only celestial bodies' gravity, but also the pressure of sunlight and the solar wind. But they have gotten very good at that, and they also maintain very precise ephemerides, tables of the celestial bodies' positions. One can use spacecraft navigation data as inputs for those also.
