Control design for orbital reentry of a winged space vehicle, involving variation of the angle of roll

Details Control design for orbital reentry of a winged space vehicle, involving variation of the angle of roll Control design for orbital reentry of a winged space vehicle, involving variation of the angle of roll

Jan 1977

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1977kosis..15...34n&link_type=abstract

Kosmicheskie Issledovaniia, vol. 15, Jan.-Feb. 1977, p. 34-41. In Russian.

Physics

Descent Trajectories, Lateral Control, Numerical Control, Spacecraft Reentry, Trajectory Optimization, Algorithms, Monte Carlo Method, Spacecraft Maneuvers, Time Optimal Control, Winged Vehicles

Scientific paper

In the reentry control discussed, the angle of roll is the controlling parameter. Methods are proposed for obtaining nominal control programs and also control laws in which the coefficients are optimal with respect to the accuracy criterion. The algorithm described is particularly well suited for reentry control systems designed for weight and volume constraints.

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