Abstract
For an interception strategy of a removable target by a return space vehicle (RSV), we propose a structure of the control law by the aerodynamic efficiency that determines a chain of the three standard trajectories: nosing-up–free flight–nosing-down. A solution of the terminal problem is to determine numerical values of the control parameters that define moments to switch the RSV flight from one standard trajectory to another.
This is a preview of subscription content, log in via an institution to check access.
Similar content being viewed by others
References
Afanas’ev, V.A. and Khairullin, V.R., On Synthesizing the FV Control with the Use of Analytical Equations of Motion, Vestnik KGTU im. A.N. Tupoleva, 2009, no. 3, pp. 98–102.
Afanas’ev, V.A., Meshchanov, A.S., and Khairullin, V.R., Analytical Synthesis of Controls by Re-Entry Space Vehicles with the Use of the Typical Path Conjugation Method, Vestnik KGTU im. A.N. Tupoleva, 2009, no. 4, pp. 96–102.
Afanas’ev, V.A., Meshchanov, A.S., and Khairullin, V.R., Analytical Design of Re-Entry SV Flight Paths, Vestnik KGTU im. A.N. Tupoleva, 2010, no. 4, pp. 161–170.
Afanas’ev, V.A., Meshchanov, A.S., and Khairullin, V.R., Model Problem on FV Interception in the Homogeneous Atmosphere, Vestnik KGTU im. A.N. Tupoleva, 2010, no. 2, pp. 118–121.
Author information
Authors and Affiliations
Corresponding author
Additional information
Original Russian Text © V.A. Afanas’ev, G.L. Degtyarev, A.S. Meshchanov, 2016, published in Izvestiya VUZ, Aviatsionnaya Tekhnika, 2016, No. 1, pp. 15–21.
About this article
Cite this article
Afanas’ev, V.A., Degtyarev, G.L. & Meshchanov, A.S. Analytical construction of interception trajectories in atmosphere. Russ. Aeronaut. 59, 15–22 (2016). https://doi.org/10.3103/S1068799816010037
Received:
Published:
Issue Date:
DOI: https://doi.org/10.3103/S1068799816010037