Fault-tolerance in distributed digital fly-by-wire flight control systems
Spacecraft 2000 - the challenge of the future
Progress in knowledge-based flight monitoring
Microprocessor controlled and managed fly-by-wire hydraulic actuator
An auxiliary navigation system for an autonomous underwater vehicle
Three-phase AC traction drives: design and service experience
Development process for automotive sensors
Reliability testing of the fault tolerant spacecraft computer (final rept.)
A measure of reliability for classification of Earth satellite data
Charging of spacecraft by nuclear electrons
Requirements for sole means navigation in U.S. navy aircraft
Telerobotic work system-space robotics application
Interface design considerations for F-16 sensors and weapons
Spacecraft charging effects by the high-energy natural environment
VII, IFAC sympos. on automatic control in space, rottach-egern (FRG), 17-21 may, 1976
Introduction of the ground proximity warning system (GPWS) into airline service
Fault-tolerant computer system design using GRAMP
Design for reliability/availability The An/Spy-1 Radar system
Multiple access model for emergency position indicating radio beacons
A long awaited capibility, lessons learned and projections
Embedded stress transducers for solid propellant rocket motor applications
Performance and economy of a fault-tolerant multiprocessor
Integrated strapdown avionics for precision guided weapons
Modularity - as implemented on DSCS III and BSE satellites
Einsatz von SM-Technologien in der Luftfahrt
Autocalibration of a laser gyro strapdown inertial reference/navigation system
Failure mode, effect and criticality analysis
A flight control system using the DIAS archiecture
Current developments in the design of air defence ground radar systems
'LEA' microwave approach and landing system
The role of system performance analysis in the independent assessment of B1-navigation software
Automatic vehicle location. Dallas test results
Expert system applications to the cockpit of the '90S