Design framework for optimizing waypoints of vehicle trajectory considering terminal velocity and impact angle constraints

References

• Callaway, D. W. 2004. “Coplanar Air Launch with Gravity-Turn Launch Trajectories.” MS thesis, Department of Aeronautics and Astronautics, Air Force Institute of Technology, Wright–Patterson Air Force Base. Dayton, OH: Storming Media.
   Google Scholar
• Chandler, D. C., and I. E. Smith. 1967. “Development of the Iterative Guidance Mode with Its Application to Various Vehicles and Missions.” Journal of Spacecraft and Rockets 4 (7): 898–903.
   Web of Science ®Google Scholar
• Chen, Si-Yuan, and Qun-Li Xia. 2016. “A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles.” International Journal of Aerospace Engineering 2016: Article ID 6346742. doi:https://doi.org/10.1155/2016/6346742.
   Google Scholar
• Eggers, A. J. 1957. “Performance of Long Range Hypervelocity Vehicles.” Journal of Jet Propulsion 27 (11): 1147–1151.
   Google Scholar
• Guo, Yanning, Matt Hawkins, and Bong Wie. 2013. “Waypoint-Optimized Zero-Effort-Miss/Zero-Effort-Velocity Feedback Guidance for Mars Landing.” Journal of Guidance, Control, and Dynamics 36 (3): 799–809.
   Web of Science ®Google Scholar
• He, Shaoming, Chang-Hun Lee, Hyo-Sang Shin, and Antonios Tsourdos. 2019. “Minimum-Effort Waypoint-Following Guidance.” Journal of Guidance, Control, and Dynamics 42 (7): 1551–1561.
   Web of Science ®Google Scholar
• Jorris, Timothy R., and Richard G. Cobb. 2009. “Three-Dimensional Trajectory Optimization Satisfying Waypoint and No-Fly Zone Constraints.” Journal of Guidance, Control, and Dynamics 32 (2): 551–572.
   Web of Science ®Google Scholar
• Kim, Sangjae, and Taeyoon Um. 2015. “Flight-Path Angle Control for Cutoff Insensitive Guidance.” Journal of Guidance, Control, and Dynamics 38 (4): 706–710.
   Web of Science ®Google Scholar
• Kraemer, J. W., and H. L. Ehlers. 1975. “Shuttle Orbiter Guidance System for the Terminal Flight Phase.” IFAC Proceedings Volumes 8 (1), Part 4: 328–337. doi:https://doi.org/10.1016/S1474-6670(17)67485-8.
   Google Scholar
• Kuroda, T., and F. Imado. 1997. “A Mid-Course Guidance Law for Highly Maneuverable Thrust Vector Control Missiles.” In AIAA Guidance, Navigation, and Control Conference. Reston, VA: American Institute of Aeronautics and Astronautics.
   Google Scholar
• Lan, Xuejing, Wenbiao Xu, and Yongji Wang. 2020. “3D Profile Reconstruction and Guidance for the Terminal Area Energy Management Phase of An Unpowered RLV with Aerosurface Failure.” Journal of Aerospace Engineering 33 (3): Article ID 04020003. doi:https://doi.org/10.1061/(ASCE)AS.1943-5525.0001112.
   Google Scholar
• Liang, Zixuan, Qingdong Li, and Zhang Ren. 2016. “Waypoint Constrained Guidance for Entry Vehicles.” Aerospace Science and Technology 52: 52–61.
   Web of Science ®Google Scholar
• Lu, Ping. 2014. “Entry Guidance: A Unified Method.” Journal of Guidance, Control, and Dynamics 37 (3): 713–728.
   Web of Science ®Google Scholar
• McHenry, R. L., A. D. Long, B. F. Cockrell, J. R. Thibodeau III, and T. J. Brand. 1979. “Space Shuttle Ascent Guidance, Navigation, and Control.” Journal of the Astronautical Sciences 27 (1): 1–38.
   Web of Science ®Google Scholar
• Moon, K., S. Park, and C. Ryoo. 2015. “Guidance Algorithm for Satisfying Terminal Speed and Impact Angle Constraints with the Neural Network Technique.” In Proceedings of the 15th International Conference on Control, Automation and Systems (ICCAS), 466–471. Piscataway, NJ: IEEE. doi:https://doi.org/10.1109/ICCAS.2015.7364962.
   Google Scholar
• Perkins, F. M. 1966. Derivation of Linear-Tangent Steering Laws. Air Force Report No. SSD-TR-66-211. Air Force Systems Command, Los Angeles, CA. https://apps.dtic.mil/dtic/tr/fulltext/u2/643209.pdf.
   Google Scholar
• Rafique, A. F., L. S. He, Q. Zeeshan, A. Kamran, and K. Nisar. 2011. “Multidisciplinary Design and Optimization of An Air Launched Satellite Launch Vehicle Using a Hybrid Heuristic Search Algorithm.” Engineering Optimization 43 (3): 305–328. doi:https://doi.org/10.1080/0305215X.2010.489608.
   Web of Science ®Google Scholar
• Ryoo, Changkyung, Hangju Cho, and MinJea Tahk. 2005. “Optimal Guidance Laws with Terminal Impact Angle Constraint.” Journal of Guidance, Control, and Dynamics 28 (4): 724–732.
   Web of Science ®Google Scholar
• Shirazi, Abolfazl. 2016. “Trajectory Optimization of Spacecraft High-Thrust Orbit Transfer Using a Modified Evolutionary Algorithm.” Engineering Optimization 48 (10): 1639–1657. doi:https://doi.org/10.1080/0305215X.2015.1115026.
   Web of Science ®Google Scholar
• Tahk, M. J., G. H. Moon, and S. W. Shim. 2019. “Augmented Polynomial Guidance with Terminal Speed Constraints for Unpowered Aerial Vehicles.” International Journal of Aeronautical and Space Sciences 20 (1): 183–194.
   Web of Science ®Google Scholar
• Wang, R., S. Tang, and D. Zhang. 2019. “Short-Range Reentry Guidance with Impact Angle and Impact Velocity Constraints for Hypersonic Gliding Reentry Vehicle.” IEEE Access 7: 47437–47450.
   Web of Science ®Google Scholar
• White, J. E. 1993. “Cut-Off Insensitive Guidance with Variable Time of Flight.” In Proceedings of the AIAA Guidance and Control Conference. Reston, VA: American Institute of Aeronautics and Astronautics. doi:https://doi.org/10.2514/6.1993-3785.
   Google Scholar
• Williamson, W. E., R. W. Greene, and D. G. Hull. 1976. “Application of the Perturbation Method to Optimal Shuttle Reentry Trajectories.” Engineering Optimization 2 (3): 189–196. doi:https://doi.org/10.1080/03052157608960611.
   Google Scholar
• Zarchan, Paul. 1990. Tactical and Strategic Missile Guidance. 3rd ed. Vol. 176 of Progress in Astronautics and Aeronautics. Washington, DC: American Institute of Aeronautics and Astronautics.
   Google Scholar
• Zhou, H., T. Rahman, and W. Chen. 2015. “Impact Angle and Impact Velocity Constrained Terminal Guidance for Stationary Target.” Aircraft Engineering and Aerospace Technology 87: 454–464.
   Web of Science ®Google Scholar