journal article·2022-06-24Open access

Rapid Construction of Aerocapture Attainability Sets Using Sequential Convex Programming

Rui Teng, Hongwei Han, Jilin Chen

Applied Sciences· Volume 12· Issue 13

Abstract

This paper proposes a novel method to efficiently construct the aerocapture attainability set based on convex optimization. Using dimensionality reduction, constructing the attainability set is equivalent to solving a set of discrete points on its boundary. As solving each of the boundary points is a typical nonlinear optimal control problem, a sequential convex programming method is adopted. The efficiency and accuracy of the proposed algorithm is demonstrated by high-fidelity numerical results. This is the first time that the configuration of the aerocapture attainability set is precisely described by the state variables at atmospheric exit. Since the quantification of the set is significant for assessing the feasibility of performing an aerocapture maneuver, the proposed method can be used as a reliable tool for systematic design for aerocapture mission.
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Research context

OpenAlex topics: Spacecraft Dynamics and Control · Space Satellite Systems and Control · Robotic Path Planning Algorithms

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100811, China

Funding

National Natural Science Foundation of China

References (53)

Show source-provided references
1. Parametric study of aerocapture for missions to Venus10.2514/1.2589 ↗
2. Han, H., Qiao, D., and Chen, H. (2016, January 12–14). Optimal ballistic coefficient control for Mars aerocapture. Proceedings of the 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC), Nanjing, China.
3. Improvement to the analytical predictor-corrector guidance algorithm applied to Mars aerocapture10.2514/1.20126 ↗
4. Fuel-optimal bank-angle control for lunar-return aerocapture10.2514/3.26587 ↗
5. Drag-modulation flight-control system options for planetary aerocapture10.2514/1.A32589 ↗
6. Preliminary studies on the planetary entry to Jupiter by aerocapture technique10.1016/j.actaastro.2005.07.034 ↗
7. Optimization for the aeroassisted orbital plane change with the synergetic maneuver using the hp-adaptive pseudospectral method10.1061/(ASCE)AS.1943-5525.0000788 ↗
8. Development of optimal and robust predictive guidance technique for Mars aerocapture10.1016/j.ast.2013.07.012 ↗
9. Energy-saving capture at Mars via backward stable orbits10.2514/1.G004006 ↗
10. Utilization of libration points for human exploration in the Sun–Earth–Moon system and beyond10.1016/j.actaastro.2004.05.021 ↗
11. Angular momentum analysis in the elliptic restricted three-body problem10.1093/mnras/stac763 ↗
12. Mars high orbit capture using manifolds in the sun–mars system10.2514/1.G004865 ↗
13. Analysis of capture trajectories into periodic orbits about libration points10.2514/1.33796 ↗
14. Analysis of two-impulse capture trajectories into halo orbits of Sun-Mars system10.2514/1.62272 ↗
15. Stability analysis of Earth co-orbital objects10.3847/1538-3881/ac5e2c ↗
16. Nonlinear station-keeping control in the vicinity of the sun-earth l2 point using solar radiation pressure10.1061/(ASCE)AS.1943-5525.0000553 ↗
17. Armellin, R., Lavagna, M., and Ercoli-Finzi, A. (2006). Aero-gravity assist maneuvers: Controlled dynamics modeling and optimization. Periodic, Quasi-Periodic and Chaotic Motions in Celestial Mechanics: Theory and Applications, Springer.10.1007/s10569-006-9024-y ↗
18. Flight-path angle guidance for aerogravity-assist maneuvers on hyperbolic trajectories10.2514/1.G000670 ↗
19. Optimal aerogravity-assist trajectories minimizing total heat load10.2514/1.G002467 ↗
20. Stiles, J. (1970, January 2–6). Predictive entry guidance for an Apollo-type vehicle. Proceedings of the 3rd International IFAC Conference on Automatic Control in Space, Toulouse, France.10.1016/S1474-6670(17)68824-4 ↗
21. The 1st John V. Breakwell Memorial Lecture: Recent advances in the optimization and guidance of aeroassisted orbital transfers10.1016/S0094-5765(96)00076-8 ↗
22. Atmospheric guidance concepts for an aeroassist flight experiment
23. Masciarelli, J., Rousseau, S., Fraysse, H., and Perot, E. (2000, January 14–17). An analytic aerocapture guidance algorithm for the Mars Sample Return Orbiter. Proceedings of the Atmospheric Flight Mechanics Conference, Denver, CO, USA.10.2514/6.2000-4116 ↗
24. Graves, C., and Masciarelli, J. (2013, January 19–22). An analytical assessment of aerocapture guidance and navigation flight demonstration for applicability to other planets. Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit, Boston, MA, USA.
25. Virtual terminal–based adaptive predictor–corrector entry guidance10.1061/(ASCE)AS.1943-5525.0000716 ↗
26. Starr, B., and Westhelle, C. (2005, January 15–18). Aerocapture Performance analysis of a Venus explorer mission. Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit, San Francisco, CA, USA.10.2514/6.2005-5913 ↗
27. Blended control, predictor–corrector guidance algorithm: An enabling technology for Mars aerocapture10.1016/S0094-5765(03)00159-0 ↗
28. Optimal aerocapture guidance10.2514/1.G000713 ↗
29. Masciarelli, J., Westhelle, C., and Graves, C. (2004, January 16–19). Aerocapture guidance performance for the neptune orbiter. Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit, Providence, RI, USA.10.2514/6.2004-4954 ↗
30. Vehicle/trajectory optimization for aerocapture at Mars
31. Sigal, E., and Guelman, M. (2001, January 1–5). Optimal aerocapture with minimum total heat load. Proceedings of the 52nd International Astronautical Congress, Toulouse, France.
32. Multidisciplinary optimization of aerocapture maneuvers
33. Knittel, J., and Lewis, M. (2012, January 24–28). Multidisciplinary optimization of starbody waverider shapes for lifting aerocapture with orbital plane change. Proceedings of the 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France.10.2514/6.2012-5809 ↗
34. Exploiting sparsity in direct collocation pseudospectral methods for solving optimal control problems10.2514/1.A32071 ↗
35. Optimization and guidance of trajectories for coplanar, aeroassisted orbital transfer
36. Unified multiobjective optimization scheme for aeroassisted vehicle trajectory planning10.2514/1.G003189 ↗
37. Convex programming approach to powered descent guidance for Mars landing10.2514/1.27553 ↗
38. Minimum-landing-error powered-descent guidance for Mars landing using convex optimization10.2514/1.47202 ↗
39. Autonomous trajectory planning for rendezvous and proximity operations by conic optimization10.2514/1.58436 ↗
40. Entry trajectory optimization by second-order cone programming10.2514/1.G001210 ↗
41. Rapid path planning for zero-propellant maneuvers10.1061/(ASCE)AS.1943-5525.0000542 ↗
42. Rapid path planning for zero propellant maneuvers based on flatness10.1061/(ASCE)AS.1943-5525.0000753 ↗
43. Survey of convex optimization for aerospace applications10.1007/s42064-017-0003-8 ↗
44. Minimum-Fuel low-thrust trajectory optimization via reachability analysis and convex programming10.2514/1.G004766 ↗
45. Coast arcs in optimal multiburn orbital transfers10.2514/1.54655 ↗
46. Double-homotopy method for solving optimal control problems10.2514/1.G001553 ↗
47. Safe rendezvous scenario design for geostationary satellites with collocation constraints10.1007/s42064-017-0006-5 ↗
48. Entry Guidance: A unified method10.2514/1.62605 ↗
49. Precise determination of reachable domain for spacecraft with single impulse10.2514/1.G000583 ↗
50. Reachable domain for spacecraft with ellipsoidal delta-v distribution10.1007/s42064-018-0025-x ↗
51. Primal-Dual Interior-Point Methods for Self-Scaled Cones10.1137/S1052623495290209 ↗
52. MOSEK, A. (2022, May 29). The MOSEK Optimization Toolbox for MATLAB Manual. Version 7.1 (Revision 28). Available online: http://docsmosekcom/71/toolbox/indexhtml.
53. Rapid planning for aerocapture trajectory via convex optimization10.1016/j.ast.2018.11.009 ↗