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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