Interplanetary spacecraft navigation and guidance : mechanics of probe entry and ballistic transfers to sun-earth Lagrange L₁ halo orbits /
Interplanetary Spacecraft Navigation and Guidance examines a vast field that was developed to enable the exploration of the moon and planets in the solar system by increasingly sophisticated spacecraft, flying-by, landing or orbiting the inner and outer planets and releasing probes to enter their at...
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| Format: | Book |
| Language: | English |
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Reston, Virginia :
American Institute of Aeronautics and Astronautics,
[2025].
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| Series: | Progress in astronautics and aeronautics ;
v. 272. |
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Table of Contents:
- Preface
- Information content of radiometric and optical data during planetary encounter
- Orbit determination accuracy assessment for an asteroid flyby: a Galileo case study
- Error analysis for hyperbolic entry into planetary atmosphere
- The mathematical description of the JPL Station location error covariance and the covariance mapping programs used to generate a priori error covariances and map state error covariances to entry parameters
- Galileo probe trajectory reconstruction accuracy analysis
- Three-body orbit mechanics and generation of Lagrange L₁ halo orbits
- The computation of ballistic transfer trajectories from low Earth orbit to Sun-Earth L₁ libration point halo orbit
- Transfer trajectories from low Earth orbit to a large L₁-centered class I halo orbit in the Sun-Earth circular problem using a constrained insertion mode
- Local regularization of the restricted elliptic three-body problem in rotating coordinates
- Solar survaillance zone population strategies with picosatellites using halo and distant retrograde orbits
- Index
- Supporting materials.