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IssuesArchive of Issues2019-3pp.474-485

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A.V. Molodenkov and Ya.G. Sapunkov, "Analytical Quasi-Optimal Solution for the Problem on Turn Maneuver of an Arbitrary Solid with Arbitrary Doundary Conditions," Mech. Solids. 54 (3), 474-485 (2019)
Year 2019 Volume 54 Number 3 Pages 474-485
DOI 10.3103/S0025654419020110
Title Analytical Quasi-Optimal Solution for the Problem on Turn Maneuver of an Arbitrary Solid with Arbitrary Doundary Conditions
Author(s) A.V. Molodenkov (Institute for Precision Mechanics and Control of the Russian Academy of Sciences, ul. Rabochaya 24, Saratov, 410028 Russia, molalexei@yandex.ru)
Ya.G. Sapunkov (Institute for Precision Mechanics and Control of the Russian Academy of Sciences, ul. Rabochaya 24, Saratov, 410028 Russia)
Abstract The problem of energy-optimal turn maneuver of a solid having arbitrary dynamic configuration is considered within the framework of the quaternion formulation with arbitrary boundary conditions and without restrictions imposed on the control function. This turn maneuver is performed in fixed time. In the class of generalized conical motions, the optimal turn maneuver problem has been modified. As a result, it is possible to obtain its analytical solution. The analytical solution of the modified problem can be considered as an approximate (quasi-optimal) solution of the traditional optimal turn maneuver problem. An algorithm for the quasi-optimal turn maneuver of a solid is given. Given numerical examples illustrate that the solution of the modified problem is a close approximation for the solution of the traditional problem on the optimal turn maneuver of a solid. In addition, the examples show that the kinematic characteristics of the optimal motion in the traditional problem (attitude quaternion and angular velocity vector) depend weakly on the dynamic configuration of a solid and are mainly determined by the boundary conditions of the problem (anyway, for |φ|≤π/2 where φ is the Euler angle). The weak dependence of the kinematic characteristics of the optimal motion of a solid on its dynamic configuration guarantees the closeness of the solutions of the modified and traditional problems of optimal turn maneuver of a body with an arbitrary dynamic configuration.
Keywords solid, optimal turn maneuver, quasi-optimal solution, generalized conic motion, arbitrary boundary conditions, spacecraft
Received 10 March 2017
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