Results 271 to 280 of about 500,409 (312)
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Path shaping guidance for terminal lunar descent
Acta Astronautica, 1995Abstract Lunar descent guidance methods are investigated which provide soft landing in regions of undulating terrain. Path shaping guidance is developed to provide a family of descent paths which converge to a soft-landing, but avoid obstructions created by neighbouring terrain.
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Terminal Guidance Law Based on Proportional Navigation
Journal of Guidance, Control, and Dynamics, 2005Introduction A TOPIC of classical interest in atmospheric flight dynamics of a landing aircraft or lifting-body vehicle is the synthesis of flight path from an arbitrary initial point to a terminal point with a desired final velocity vector direction.
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Reentry Terminal Guidance Through Sliding Mode Control
Journal of Guidance, Control, and Dynamics, 2010A guidance scheme has been developed for the terminal guidance of an unpowered lifting reentry vehicle during the approach and landing phase. The proposed approach is quite useful for offline trajectory design and allows for trajectories to be generated online through the use of a closed-loop control law.
Nathan Harl, S. N. Balakrishnan
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Terminal Guidance for Continuous Powered Space Vehicles
AIAA Journal, 1966Error correcting problem in space trajectory of continuous powered space vehicle, discussing optimal terminal ...
B. D. TAPLEY, W. T. FOWLER
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Failure Mode Analysis of Terminal Guidance Projectile
2019 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE), 2019The structure of terminal guidance projectiles is complex, the technology is high, and the possible reasons for the failure in operational use are also very complicated. In this paper, according to three kinds of accidents that occurred when live firing, and combined with the structure and principle, fault tree analysis was used to analyze its failure ...
Meng Gao +4 more
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Terminal-Set-Based Optimal Stochastic Guidance
2023 31st Mediterranean Conference on Control and Automation (MED), 2023Liraz Mudrik, Yaakov Oshman
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Lambda matrix terminal control for missile guidance.
Journal of Spacecraft and Rockets, 1968(Gordon and Breach Science Publishers, New York, 1966), Vol. I, p. 247. 2 Eichelberger, R. J., "Hypervelocity impact," Behavior of Materials Under Dynamic Loading (American Society of Mechanical Engineers, New York, 1965), p. 155. 3 Rae, W. J. and Kirchner, H. P., "A study of meteoroid impact phenomena," Cornell Aeronautical Lab. Inc., Rept. RM-1655M-4
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Euler Elastica Terminal Parafoil Guidance
24th AIAA Aerodynamic Decelerator Systems Technology Conference, 2017Patrick Handley +4 more
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An optimal terminal guidance law
IEEE Transactions on Automatic Control, 1976openaire +1 more source