Space shuttle guidance during approach and landing
Approach trajectories and guidance concepts for space shuttle approach and landing
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Approach trajectories and guidance concepts for space shuttle approach and landing
Factors influencing guidance accuracy of planetary probes
Guidance laws for controlling LM powered descent trajectories
Approach guidance method using single onboard optical measurement
Designing terminal area navigation, guidance, and control system suitable for landing space shuttle vehicles under Category 2 conditions
Space mission flight guidance modes analysis and evaluation
Flight test experiments for H-19 helicopter to evaluate aided inertial system performance for terminal guidance
Trajectory, guidance and environmental parameters and uncertainties effect on design optimization of out-of-orbit Viking soft lander
Ground-based and onboard guidance and navigation systems for outer planet flyby missions concerning direct, Jupiter swingby and Grand Tour trajectories
Subsonic glide landing approach guidance for unpowered lifting vehicles, using perturbation feedback and approximation of heading and position coordinates
Linearized theory for minimum fuel guidance in neighborhood of minimum fuel space trajectory, unrestricted thrust magnitude and allowances for midcourse impulses
Minimum fuel control for discrete time Gaussian processes, applying results to spacecraft midcourse guidance for earth-Mars mission
Mariner Mars 1969 navigation, guidance and control systems design, mechanization and flight testing
Radio command guidance system for Mars probe ascent from surface to rendezvous with flyby vehicle on escape trajectory
Terminal constraints affecting matrices comprising linear impulsive guidance law for earth approach, discussing Mars mission
Laser tracking system for space guidance, describing equipment and operations
Wind effects on rigid launch vehicle guidance and control system design, using model incorporating structural bending and fuel sloshing
Flight test experiments for H-19 helicopter to evaluate aided inertial system performance for terminal guidance