Verification of performance of the LM guidance and control systems.
LM guidance and control systems performance verification
SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
LM guidance and control systems performance verification
Performance errors analysis of navigation using inertial guidance and radar tracking
Optimization of Saturn vehicle, considering interaction of guidance, control and propellant utilization systems
Surveyor guidance program for midcourse and terminal information, noting redundancy in design, decision making telecommunications, etc
Feedback from observations introduced into midcourse guidance correction program, showing optimal random feedback solution obtained for deterministic optimal feedback control problems
Navigation and guidance analysis of Mars probe launched from manned flyby spacecraft for 1975- 1976
Application of redundancy in Saturn V guidance and control system to achieve desired reliability
Apollo gyro reliability covering Guidance, Navigation and Control systems, stressing failure mode prediction
Manual optimal guidance scheme using predictive display applied to launch vehicles during boost for continuous generation of predicted fuel- optimal trajectory
Guidance system requirements for unmanned Martian propulsive landing capsule
Iterative guidance mode /IGM/ applied to effective gravity vector prediction, acceleration measurement of noise sensitivity and energy limitations
Onboard computer equations for rocket vehicle guidance to elliptical orbit, discussing iteration absence from computations and digital simulation results
Mars landing guidance requirements for unmanned lander after separation from interplanetary flyby space vehicle
Iterative guidance mode, deriving alternate expressions for thrust direction control angle for time savings on Saturn launches
Suboptimal feedback solution to guidance and control in minimum time and fuel for low thrust orbital transfer
Terminal guidance problem involving optimal control for deviations in systems with transport lag
None given. This presentation was made to help develop new mini/micro guidance and control system architectures and components that meet the needs of future space systems.
In this paper, we address the atmospheric entry guidance and control problem for Mars precision landing.