Call for Paper - January 2023 Edition
IJCA solicits original research papers for the January 2023 Edition. Last date of manuscript submission is December 20, 2022. Read More

Multidisciplinary Design Optimization of a Deorbit Maneuver Considering Propulsion, TPS, and Trajectory

Print
PDF
International Journal of Computer Applications
© 2015 by IJCA Journal
Volume 116 - Number 23
Year of Publication: 2015
Authors:
Amirhossein Adami
Mahdi Mortazavi
Mehran Nosratollahi
10.5120/20496-2109

Amirhossein Adami, Mahdi Mortazavi and Mehran Nosratollahi. Article: Multidisciplinary Design Optimization of a Deorbit Maneuver Considering Propulsion, TPS, and Trajectory. International Journal of Computer Applications 116(23):1-6, April 2015. Full text available. BibTeX

@article{key:article,
	author = {Amirhossein Adami and Mahdi Mortazavi and Mehran Nosratollahi},
	title = {Article: Multidisciplinary Design Optimization of a Deorbit Maneuver Considering Propulsion, TPS, and Trajectory},
	journal = {International Journal of Computer Applications},
	year = {2015},
	volume = {116},
	number = {23},
	pages = {1-6},
	month = {April},
	note = {Full text available}
}

Abstract

Unguided reentry capsules are usually involved in ballistic entry. The final states (such as altitude and velocity of parachute activity) depend on initials parameters. Reentry trajectory parameters differently affect the thermal protection system (TPS), required deorbit propellant, and structural load. The purpose of this paper is to optimal design of deorbit parameters to minimize the thermal protection system mass and deorbit propellant mass using multidisciplinary design optimization technique. Genetic Algorithm (GA) is used to simultaneously optimize TPS discipline, propulsion discipline and trajectory in present of the all trajectory and configuration constraints. To do this, every discipline is mathematically modeled. A suitable framework of Multidisciplinary design optimization (MDO) is developed. Then, the reentry mission is optimized according to the each discipline. The results show that simultaneous optimization is more efficient in comparison with single discipline optimization such as TPS optimization or deorbit propulsion system (propulsion and propellant) optimization.

References

  • Multidisciplinary Design Optimization of RLV Reentry Trajectory. Chen Gang, Xu Min and et al. . , AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies, 2005. AIAA 2005-3270.
  • optimal skips entry into atmosphere with minimum heat. Istratie, Vasile. Austin, Texas : AIAA Atmospheric Flight AIAA Atmospheric Flight, 11-14 August, 2003. .
  • Aerodynamic stability of reentry heat shield shapes for a crew exploration vehicle. J. E. Johnson and et. al. , No. 4, Journal of Spacecraft and Rockets, July-Aug 2006, Vol. 43.
  • Hypersonic Aerothermodynamics/Aerothermoelastics Methodology for Reusable Launch Vehicles/TPS Design and Analysis. Liu D. , Chen P. , Tang L. , and Chang K. , 41st Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 6-9, 2003. AIAA-2003-897.
  • Trajectory and Thermal Protection System Design for Reusable Launch Vehicles. McGuire M. , Gage P. , Galloway E. , Huynh L. , 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany, New York, Aug. 30-1, 2004. AIAA Paper 2004-4490.
  • Aerodynamic Shape Optimization of a Re-entry Capsule. Rajesh Kumar Arora, Pradeep Kumar. , AIAA Atmospheric Flight Mechanics Conference and Exhibit, Austin, Texas, 11 - 14 August 2003.
  • Multidisciplinary design optimization of a re-entry vehicle shape and trajectory. M. Tava, S. Suzuki, 2001. AIAA-2001-1920.
  • Multidisciplinary design optimization of a reentry vehicle using genetic algorithm. M. Nosratollahi, M. Mortazavi, A. Adami, M. Hosseini, Aircraft Engineering and Aerospace Technology, 2010, Vol. 82, No:3, pp. 194-203.
  • Multidisciplinary Design Optimization of a Controllable Reentry Capsule for minimum Landing velocity. M. Nosratolahi, M. Hoseini, A. Adami. 51st AIAA/ASME/ ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Florida , 12–15 April 2010. AIAA-2010-3009.
  • Multidisciplinary Design Optimization of a Manned Reentry Mission Considering Trajectory and Aerodynamic Configuration. Amirhossein Adami, Mehdi Mortazavi, Mehran Nosratollahi, Majid Hosseini, International Conference on Recent Advances in Space Technologies, Stanbul, Turkye, 09-11 June 2011.
  • Adami, Amirhossein. Multidicsiplinary design optimization of Reentry Vehicle considering Guidance Algorithm. Aerospace Department. Tehran, Iran , Amirkabir University of Technology, 2014. Ph. d thesis.
  • Multidisciplinary Design Optimization of Hydrogen Peroxide Monopropellant Propulsion System using GA and SQP. Adami Amirhossein, Mortazavi Mahdi and Nosratollahi Mehran. 9, March 2015, International Journal of Computer Applications, Vol. 113, pp. pp. 14-21.