Adaptive Algorithm for Controlling the Soft Vertical Landing of an Unmanned Return Spacecraft. I.
Analytical construction of interception trajectories in atmosphere
Analytical Design of the Law for Control of the Center of Mass Motion for an Unmanned Aerial Vehicle
Controlling of a return space vehicle along transition trajectories in atmosphere
Control of flight vehicles with the adjustable center of mass
Control of spacecraft turns in scheduled time using rocket engines
Landing of flight vehicles without the landing gear
Roll control of a flight vehicle with the adjustable center of mass