Pages that link to "Item:Q394076"

The following pages link to The use of the exact pole placement algorithm for the control of spacecraft motion (Q394076):

Displaying 11 items.

• Synthesis of decoupling laws for controlling the angular motion of landing module with solid-fuel landing engine minimizing the transient time (Q393690) (← links)
• Application of generalized Butterworth polynomials for stabilization of the equilibrium position of a space station (Q786175) (← links)
• Asymptotic behavior of solutions of Lorenz-like systems: analytical results and computer error structures (Q1696065) (← links)
• Output control of the longitudinal motion of a flying vehicle (Q1742397) (← links)
• Electrodynamic stabilization of artificial Earth satellites in the König coordinate system (Q1743046) (← links)
• Methods for the vibration determination and parameter identification of spacecraft with flexible structures (Q1745820) (← links)
• Terminal synthesis of orbital orientation for a spacecraft (Q1745868) (← links)
• Algorithms for the synthesis of observers for nonlinear dynamic systems (Q2017643) (← links)
• Terminal bang-bang impulsive control of linear time invariant dynamic systems (Q2263914) (← links)
• Delayed feedback stabilization and the Huijberts-Michiels-Nijmeijer problem (Q2358673) (← links)
• (Q2983552) (← links)