Pages that link to "Item:Q1778643"
From MaRDI portal
The following pages link to Methods of estimating the envelope of elastic oscillations of the flexible spacecraft (Q1778643):
Displaying 8 items.
- Estimating nonmeasurable coordinates of elastic oscillations for large space constructions with a gyroforce engine (Q386933) (← links)
- Modal parameter identification of flexible spacecraft using the covariance-driven stochastic subspace identification (SSI-COV) method (Q529205) (← links)
- Parametric adaptation algorithm for the basic law used to control orientation of a large space structure on the base of flexible modes envelope estimation (Q612053) (← links)
- Adaptive approach with the ``fast'' model for dynamics identification and forecasting problems for relay control of an elastic satellite (Q612073) (← links)
- A mathematical model for the angular motion of large space structures with gyroscopic drive for an active compensation of elastic oscillations (Q656265) (← links)
- Some questions of control of the robotized in-orbit assembly of large space structures (Q885729) (← links)
- On the stability of a spacecraft with regard for its elastic oscillations (Q1881967) (← links)
- Using the method of phase biplane to study dynamics of interactions of the elastic structural oscillations of the flexible spacecraft with the control system (Q2371583) (← links)
