By Angelo Miele, Aldo Frediani
Advanced layout difficulties in Aerospace Engineering, quantity 1: complicated Aerospace platforms provides six authoritative lectures at the use of arithmetic within the conceptual layout of assorted kinds of airplane and spacecraft. It covers the next issues: layout of rocket-powered orbital spacecraft (Miele/Mancuso), layout of Moon missions (Miele/Mancuso), layout of Mars missions (Miele/Wang), layout of an experimental assistance process with a standpoint flight direction show (Sachs), neighboring automobile layout for a two-stage release automobile (Well), and controller layout for a versatile airplane (Hanel/Well). it is a reference booklet of interest to engineers and scientists operating in aerospace engineering and similar issues.
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Additional info for Advanced Design Problems in Aerospace Engineering: Advanced Aerospace Systems
16-17. For further details on topics covered in this paper, see Ref. 18. 2. System Description The present study is based on a simplified version of the restricted three-body problem. More precisely, with reference to the motion of a spacecraft in Earth-Moon space, the following assumptions are employed: (A1) the Earth is fixed in space; (A2) the eccentricity of the Moon orbit around Earth is neglected; (A3) the flight of the spacecraft takes place in the Moon orbital plane; (A4) the spacecraft is subject to only the gravitational fields of Earth and Moon; the gravitational fields of Earth and Moon are central and obey (A5) the inverse square law; (A6) the class of two-impulse trajectories, departing with an accelerating velocity impulse tangential to the spacecraft velocity relative to Earth [Moon] and arriving with a braking velocity impulse tangential to the spacecraft velocity relative to Moon [Earth], is considered.
131, pp. 91-108, 1997. 15. , Recent Advances in the Optimization and Guidance of Aeroassisted Orbital Transfers, The 1st John V. Breakwell Memorial Lecture, Acta Astronautica, Vol. 38, No. 10, pp. 747-768, 1996. 16. , Robust Predictor-Corrector Guidance for Aeroassisted Orbital Transfer, Journal of Guidance, Control, and Dynamics, Vol. 19, No. 5, pp. 1134-1141, 1996. 17. , Flight Mechanics, Vol. 1: Theory of Flight Paths, Chapters 13 and 14, Addison-Wesley Publishing Company, Reading, Massachusetts, 1962.
Primal-Dual Properties of Sequential Gradient-Restoration Algorithms for Optimal Control Problems, Part 2: General Problem, Journal of Mathematical Analysis and Applications, Vol. 119, Nos. 1-2, pp. 21-54, 1986. 11. RISHIKOF, B. , McCORMICK, B. , PRITCHARD, R. , and SPONAUGLE, S. , SEGRAM: A Practical and Versatile Tool for Spacecraft Trajectory Optimization, Acta Astronautica, Vol. 26, Nos. 8-10, pp. 599-609, 1992. 12. , Optimization and Acceleration Guidance of Flight Trajectories in a Windshear, Journal of Guidance, Control, and Dynamics, Vol.
Advanced Design Problems in Aerospace Engineering: Advanced Aerospace Systems by Angelo Miele, Aldo Frediani