It is well known that in artifical satellite theory special techniques must be employed to construct a formal solution whenever the orbital inclination is sufficiently close to the critical value cos -1 (i/v/5). In this article the authors investigate the consequences of introducing certain relativi
โฆ LIBER โฆ
The problem of critical inclination combined with a resonance in mean motion in artificial satellite theory
โ Scribed by Fabienne Delhaise; Jacques Henrard
- Publisher
- Springer Netherlands
- Year
- 1993
- Tongue
- English
- Weight
- 128 KB
- Volume
- 56
- Category
- Article
- ISSN
- 1572-9478
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