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Assessing Parameters of the Coplanar Components of Perturbing Accelerations Using the Minimal Number of Optical Observations
Baranov A., Agapov V., Golosova N., Karatunov M.
and the magnitude of a velocity impulse) of a maneuver-like perturbation of motion of the center of mass of a
Assessment of Non-Coplanar Maneuver Parameters and Perturbing Accelerations Using the Minimal Number of Observations
Baranov A.
The algorithms for determining the active space object maneuver parameters in the conditions
Estimates of near-circular orbits after a single correction: a geometrical method
Baranov A.A., Vikhrachev V.O., Karatunov M.O., Razumnyi Y.N.
and numerical-analytical algorithms to estimate short-term and long-term one-impulse maneuvers for the case
Evaluation of impulsive maneuvers performed by active space object
Agapov V.M., Baranov A.A., Karatunov M.O.
The subject of this paper is the problem of estimating the maneuver parameters performed
SOLUTION OF THE EULER-LAMBERT PROBLEM BY THE OKHOTSIMSKY-EGOROV METHOD
Ивашкин В.В., Иванюхин А.В.
impulsive orbital maneuvers
Orbital maneuvers for a space probe around Titania
Xavier Jadilene, Prado A.B., Winter S.G., Amarante Andre
information about the orbited body. In this work, we present orbital maneuvers that aim to show how to avoid a
Non-Coplanar Rendezvous in Near-Circular Orbit with the Use a Low Thrust Engine
Baranov Andrey A., Olivio Adilson P.
Presented method allows one to calculate the of maneuvers performed on several turns
АЛГОРИТМ РЕШЕНИЯ ЗАДАЧИ ЭЙЛЕРА-ЛАМБЕРТА НА ОСНОВЕ МЕТОДА ОХОЦИМСКОГО-ЕГОРОВА
Ивашкин В.В., Иванюхин А.В.
, it was possible to obtain a new orbit determination method. The advantages of this method are the limitation
Coplanar multi-turn rendezvous in near-circular orbit using a low-thrust engine
Baranov Andrey A., Olivio Adilson P.
The authors describe an algorithm that allows calculating the parameters of maneuvers
DEVELOPMENT OF BALLISTIC SUPPORT FOR THE FLIGHT TO JUPITER AND ANALYSIS OF THE TRAJECTORY OF THE SPACECRAFT IN THE VICINITY OF THE PLANET
Яблоновский П.А., Бондаренко Ю.А.
circular orbit to Jupiter was calculated, followed by an analysis of maneuvers around the planet.

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