WebFeb 17, 2014 · A major breakthrough of the guidance design of TAEM vehicles can be attributed to the space shuttle entry guidance . ... J. C. Harpold and C. A. Grave, “Shuttle entry guidance,” NASA n79-74791, NASA, 1979. View at: ... “Test results for entry guidance methods for space vehicles,” Journal of Guidance, Control, and Dynamics, ... WebMay 1, 2015 · Shuttle entry guidance. J. C. Harpold, C. A. Graves; Physics. 1978; This paper describes the design of the entry guidance for the Space Shuttle Orbiter. This guidance provides the steering commands for trajectory control from initial penetration of the earth's … Expand. 371. Save.

Descent guidance and mission planning for space shuttle

WebJun 1, 2015 · Consider the Mars atmospheric entry flight, and vehicle, reference drag profile and other data from [1] are used. Later, the comparison of our law with the law in [1] will be given by simulation. The Mars lander has surface area of 16 m 2 and weighs 992 kg [19].It is assumed that the vehicle flies with trim angle of attack, and the lift-to-drag ratio and the … WebShuttle entry guidance. Harpold, J. C. ; Graves, C. A., Jr. This paper describes the design of the entry guidance for the Space Shuttle Orbiter. This guidance provides the steering … portsmouth equal

Guidance Law Design for Terminal Area Energy Management of …

http://emits.sso.esa.int/emits-doc/estec/ao-1-5636-shuttleentrygui14694.pdf WebMay 23, 2012 · Space Shuttle entry guidance performance results. Jon C. Harpold and Donald E. Gavert; Jon C. Harpold. NASA Johnson Space Center, Houston, Texas. Search … WebThe suggested guidance scheme, relying on flatness approach, is applied to the non-linear model of the European Atmospheric Re-entry Demonstrator. It is shown that the overall guidance scheme achieves robust stability and performance, even in the presence of entry point kinematics dispersions. opus holdings