Mars Entry Trajectory Planning with Range Discretization and Successive Convexification
Xu Liu, Shuang Li, Ming Xin

TL;DR
This paper introduces a convex programming approach for Mars entry trajectory planning using range discretization, improving accuracy and efficiency by transforming the problem into a series of convex sub-problems.
Contribution
It proposes a novel sequential convex programming method with range as the independent variable and new control inputs, enabling fixed-range optimization for Mars entry trajectories.
Findings
Demonstrates convergence and robustness through numerical simulations.
Achieves improved computational efficiency over traditional methods.
Validates the approach with comparative studies.
Abstract
This paper develops a sequential convex programming approach for Mars entry trajectory planning by range discretization. To improve the accuracy of numerical integration, the range of entry trajectory is selected as the independent variable rather than time or energy. A dilation factor is employed to normalize the entry dynamics and integration interval of the performance index so that the difficult free-final-time programming problem can be converted to a fixed-final-range optimization problem. The bank angle rate with respect to the range is introduced as the new control input in order to decouple the control from the state and facilitate convexification of constraints on the bank angle and its rate. The nonlinear bank angle rate constraint is further relaxed into a linear one via inequality relaxation. Moreover, the nonconvex minimum-time performance index is convexified by regarding…
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Taxonomy
TopicsSpacecraft Dynamics and Control · Aerospace Engineering and Control Systems · Space Satellite Systems and Control
