Chelnokov Yurii Nikolaevich

Publications in Math-Net.Ru

1. Quaternion models and algorithms for solving the general problem of optimal reorientation of spacecraft orbit
   
   Izv. Saratov Univ. Math. Mech. Inform., 20:1 (2020),  93–104
2. Optimal rotation of the orbit plane of a variable mass spacecraft in the central gravitational field by means of orthogonal thrust
   
   Avtomat. i Telemekh., 2019, no. 8,  87–108
3. Investigation of the problem of optimal correction of angular elements of the spacecraft orbit using quaternion differential equation of orbit orientation
   
   Izv. Saratov Univ. Math. Mech. Inform., 16:3 (2016),  336–344
4. Solving kinematic problem of optimal nonlinear stabilization of arbitrary program movement of free rigid body
   
   Izv. Saratov Univ. Math. Mech. Inform., 16:2 (2016),  198–207
5. An investigation of algorithms for estimating the inertial orientation of a moving object
   
   Izv. Saratov Univ. Math. Mech. Inform., 16:1 (2016),  80–95
6. Dual matrix and biquaternion methods of solving direct and inverse kinematics problems of manipulators for example Stanford robot arm. II
   
   Izv. Saratov Univ. Math. Mech. Inform., 14:1 (2014),  88–95
7. Dual matrix and biquaternion methods of solving direct and inverse kinematics problems of manipulators, for example Stanford robot arm. I
   
   Izv. Saratov Univ. Math. Mech. Inform., 13:4(1) (2013),  82–89
8. Solution of a Problem of Spacecraft's Orbit Optimal Reorientation Using Quaternion Equations of Orbital System of Coordinates Orientation
   
   Izv. Saratov Univ. Math. Mech. Inform., 13:1(1) (2013),  84–92
9. Analytical Solution of Linear Differential Error Equations of Strapdown Inertial Navigation System, Functioning in the Normal Geographic Reference Frame, for the Case of an Object, Following the Geographical Equator
   
   Izv. Saratov Univ. Math. Mech. Inform., 13:1(1) (2013),  69–84
10. About a problem of spacecraft's orbit optimal reorientation
    
    Izv. Saratov Univ. Math. Mech. Inform., 12:3 (2012),  87–95
11. Analytical solution of differential equations of circular spacecraft orbit orientation
    
    Izv. Saratov Univ. Math. Mech. Inform., 11:1 (2011),  84–89


12. In memory of Yakov G. Sapunkov
    
    Izv. Saratov Univ. Math. Mech. Inform., 24:3 (2024),  463–471