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Engineering topics

Lovingood, J. A.

Publications and source records attributed to Lovingood, J. A..

Shuttle ascent guidance and control.

The requirements of a unified optimal guidance scheme are discussed, giving attention to a general formulation, aspects of self-targeting, problems of optimum guidance within the atmosphere, and a unified concept for all flight phases. Since no previous guidance scheme meets these requirements, the shuttle demands a fundamentally new approach. A new unified optimal guidance scheme, called Mascot, was developed. The capabilities of Mascot include the real-time solution of general trajectory-optimization problems and the unification of guidance for all flight phases.

Lovingood, J. A.↗

Guidance and control

Wind effects on rigid launch vehicle guidance and control system design, using model incorporating structural bending and fuel sloshing

Blair, J. C.↗

Advanced control systems for launch vehicles.

Adaptive control system requirements for launch vehicles includes insensitivity to parameter variations and adjustability as function of measured flight conditions

SPACECRAFT CONTROL↗