Atmospheric entry guidance based on Differential Algebra for high elevation mars landing

Autor: Lunghi, P.; Lavagna, M.; Di Lizia, P.; Armellin , Roberto; Mease, K.D.; 

Tipo de documento: Capítulo de libro

Libro: Space Flight Mechanics Meeting, 2018

Año: 2018 

Referencias:

  • Bryson, A.E., Guidance and navigation for entry vehicles (1968) Tech. Rep. SP-8015, National Aeronautic and Space Administration
  • Harpold, J.C., Graves, C.A., Shuttle Entry Guidance (1978) American Astronautical Society, Anniversary Conference, , 25th, Houston, TX
  • Saraf, A., Leavitt, J.A., Chen, D.T., Mease, K.D., Design and Evaluation of an Acceleration Guidance Algorithm for Entry (2004) Journal of Spacecraft and Rockets, 41 (6), pp. 986-996
  • Lu, P., Predictor-corrector entry guidance for low-lifting vehicles (2008) Journal of Guidance, Control, and Dynamics, 31 (4), pp. 1067-1075
  • Prakash, R., Burkhart, P.D., Chen, A., Comeaux, K.A., Guernsey, C.S., Kipp, D.M., Lorenzoni, L.V., Way, D.W., Mars Science Laboratory Entry, Descent, and Landing System Overview (2008) IEEE Aerospace Conference 2008, pp. 1-18. , Big Sky, MT
  • Benito, J., Mease, K.D., Reachable and Controllable Sets for Planetary Entry and Landing (2010) Journal of Guidance, Control, and Dynamics, 33 (3), pp. 641-654
  • Benito, J., Mease, K., Entry trajectory planning for higher elevation landing (2008) AAS/AIAA Astrodynamics Specialist Conference 2007, Advances in the Astronautical Sciences, 129, pp. 939-958. , Univelt, San Diego, CA
  • Boada, J., Benito, J., Mease, K., (2008) Near Optimal Planner for Higher Elevation Lander, , Pegasus AIAA Student Conference, Prague, Czech Republic
  • Soler, L., Khatib, A., Mease, K., Mars Entry trajectory planning for higher elevation landing (2013) 23Rd AAS/AIAA Space Flight Mechanics Meeting, , Kauai, Hawaii
  • Lunghi, P., Armellin, R., Di Lizia, P., Lavagna, M., Semi-Analytical Adaptive Guidance Computation Based on Differential Algebra for Autonomous Planetary Landing (2016) 26Th AAS/AIAA Space Flight Mechanics Meeting, Advances in the Astronautical Sciences, 158, pp. 2003-2022. , Univelt, San Diego, CA
  • Vinh, N.X., (1981) Optimal Trajectories in Atmospheric Flight, , Elsevier, New York
  • Berz, M., (1999) Differential Algebraic Techniques, , Entry in Handbook of Accelerator Physics and Engineering, World Scientific, New York
  • Berz, M., The New Method of TPSA Algebra for the Description of Beam Dynamics to High Orders (1986) Tech. Rep. AT-6:ATN-86-16, Los Alamos National Laboratory
  • Berz, M., The Method of Power Series Tracking for the Mathematical Description of Beam Dynamics (1987) Nuclear Instruments and Methods, 258, p. 431
  • Berz, M., (1999) Modern Map Methods in Particle Beam Physics, , Academic Press, London
  • Morselli, A., Rasotto, M., Di Lizia, P., Armellin, R., Massari, M., Wittig, A., (2015) Nonlinear Propagation of Uncertainties in Space Dynamics Based on Taylor Differential Algebra, , Tech. Rep. Contract no. 4000109643/13/NL/MH Final Report, European Space Agency
  • Mendeck, G., Craig, L., Entry Guidance for the 2011 Mars Science Laboratory Mission (2011) American Institute of Aeronautics and Astronautics, , aIAA Paper 2011-6639