Deployment of Long-measured Flexible Structure in Orbit
2014
artykuł naukowy
angielski
- spacecraft
- pantograph structure
- deployment
EN Dynamics of the spacecraft with giro-gravitational system of stabilisation, in which the pantograph design deployed in an orbit and containing on the end the concentrated mass is used as the gravitational stabilizer and the carrier of solar batteries, is investigated. The analysis of the obtained information is carried out and graphs that illustrate behaviour of characteristic variables are discussed.
335 - 342
CC BY (uznanie autorstwa)
publiczny
5