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- W758622537 abstract "The steering system of the space shuttle vehicle is presented for the several hundred miles of flight preceding landing. The guidance scheme is characterized by a spiral turn to dissipate excess potential energy (altitude) prior to a standard straight-in final approach. In addition, the system features pilot oriented control, drag brakes, phugoid damping, and a navigational capacity founded upon an inertial measurement unit and an on-board computer. Analytic formulas are used to calculate, represent, and insure the workability of the system's specifications" @default.
- W758622537 created "2016-06-24" @default.
- W758622537 creator A5067781481 @default.
- W758622537 date "1973-04-09" @default.
- W758622537 modified "2023-09-24" @default.
- W758622537 title "A study of space shuttle energy management, approach and landing analysis" @default.
- W758622537 hasPublicationYear "1973" @default.
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