A method for synthesizing modal-type forced control action using a variable-structure control system

More works in this specialty

1. Formation of the architecture of an integrated navigation system for a commercial launch vehicle using GPS/GLONASS technologies

   Choi, Kyu Sun · 2003 · Candidate of Sciences

   • 05.07.09 Dynamics, ballistics, flight-motion control of aircraft
2. Improving accuracy on the basis of an adaptive predictive model of aircraft with trajectory correction

   Yao, Jun · 2000 · Candidate of Sciences

   • 05.07.09 Dynamics, ballistics, flight-motion control of aircraft
3. Development of high-accuracy guidance methods for a descent vehicle with a low lift-to-drag ratio

   Yang, Kaizhong · 1999 · Candidate of Sciences

   • 05.07.09 Dynamics, ballistics, flight-motion control of aircraft
4. Development of a vector majority redundancy method for multidimensional control systems of aircraft

   Zakharenkov, Vladilen Vasilyevich · 1999 · Candidate of Sciences

   • 05.07.09 Dynamics, ballistics, flight-motion control of aircraft
5. Optimization of maneuvers for the transfer of a spacecraft with a low-thrust engine to elliptical orbits with significant eccentricity

   Romanenko, Vladimir Alekseyevich · 1997 · Candidate of Sciences

   • 05.07.09 Dynamics, ballistics, flight-motion control of aircraft

All works in this specialty