Attitude control

Viewing 1 to 50 of 86

2010-36-0330

Study on a Fault-Tolerant System Applied to an Aerospace Control System

Neto, H. and de Oliveira e Souza, M.
SAE Technical Paper, 2010 , doi:10.4271/2010-36-0330

2007-01-2924

Generation and Customization of Real Time Code for Embedded Controllers Using a Modeling and Simulation Environment

de Amorim, F. and de Oliveira e Souza, M.
SAE Technical Paper, 2007 , doi:10.4271/2007-01-2924

2007-01-2857

Design of an Attitude Control System for the Multi-Mission Platform and its Migration to a Real Time Operating System

de Lima Bastos Moreira, M. and de Oliveira e Souza, M.
SAE Technical Paper, 2007 , doi:10.4271/2007-01-2857

2005-01-3362

A Simple Analytical Redundancy Method for Pitch and Bank Angles Estimation

Kopecki, G. and Tomczyk, A.
SAE Technical Paper, 2005 , doi:10.4271/2005-01-3362

2003-01-2641

Analysis of Thermal Design and On-Orbit Performance of the Horizon Scanners of RADARSAT-1

Wang, G., Nikanpour, D., Deraspe, G., and Nappert, S.
SAE Technical Paper, 2003 , doi:10.4271/2003-01-2641

2003-01-2274

Semi Active Roll Control Suspension (SARCS) System on a New Modified Half Car Model

Hudha, K., Jamaluddin, H., Samin, P., and Rahman, R.
SAE Technical Paper, 2003 , doi:10.4271/2003-01-2274

2001-01-2431

Thermal Design Solutions for Space Exposed P/L’s and Pointing Systems on the ISS Express Pallet

Battaglia, D., D’Angelo, F., and Nava, L.
SAE Technical Paper, 2001 , doi:10.4271/2001-01-2431

2001-01-2439

Applications of Thermal Software Coratherm to Provide Spacecraft Thermo-Elastic Inputs

Basset, T., Dudon, J., and Vernay, C.
SAE Technical Paper, 2001 , doi:10.4271/2001-01-2439

2001-01-3963

The Presence of Bifurcation in a Closed-Loop Discrete Control of a Flexible Benchmark Plant analised from the Jury Stability Criterion

Tredinnick, M., de O. e Souza, M., and Gadelha de Souza, L.
SAE Technical Paper, 2001 , doi:10.4271/2001-01-3963

2000-01-2370

Star Sensor Thermal Mode Study in Flight

Belyavskiy, E., Elchin, A., Poskonin, Y., Revzina, N. et al.
SAE Technical Paper, 2000 , doi:10.4271/2000-01-2370

2000-05-0178

An integrated semi-active suspension for passenger vehicle

Park, H. and Park, Y.
SAE Technical Paper, 2000

2000-05-0177

Development of roll attitude control theory for semi-active suspension system

Murata, M. and Ikeda, S.
SAE Technical Paper, 2000

1999-01-2851

Incorporating INS with Carrier-Phase Differential GPS for Automatic Steering Control of a Farm Tractor

Bevly, D., Rekow, A., and Parkinson, B.
SAE Technical Paper, 1999 , doi:10.4271/1999-01-2851

1999-01-2677

Solution for Direct Solar Impingement Problem on Landsat-7 ETM+ Cooler Door During Cooler Outgas in Flight

Choi, M.
SAE Technical Paper, 1999 , doi:10.4271/1999-01-2677

1999-01-2633

Design and Development of the Timed Spacecraft Solar Array

Butler, M., Dakermanji, G., Persons, D., Vernon, S. et al.
SAE Technical Paper, 1999 , doi:10.4271/1999-01-2633

1999-01-0724

Vehicle Body Attitude Control Using an Electronically Controlled Active Suspension

El-Demerdash, S., Selim, A., and Crolla, D.
SAE Technical Paper, 1999 , doi:10.4271/1999-01-0724

985517

The Feasibility of Using an INS for Control System Feedbacks

Colgren, R.
SAE Technical Paper, 1998 , doi:10.4271/985517

981891

Methodological and Empirical Approach for Cost-Benefit Analyses of Automated Vehicle Control Systems

Baum, H., Schulz, W., Geissler, T., and Schulze, M.
SAE Technical Paper, 1998 , doi:10.4271/981891

981546

Star Sensor Thermal Mode

Vitrichenko, E., Lazarev, V., Panferov, V., Poskonin, Y. et al.
SAE Technical Paper, 1998 , doi:10.4271/981546

961491

Thermal Design of the ORBCOMM Constellation Spacecraft

DeMauro, F. and Ducas, W.
SAE Technical Paper, 1996 , doi:10.4271/961491

912069

In-Flight Simulation of Backside Operating Models Using Direct Lift Controller

Tsukano, Y., Kawahata, N., Komoda, M., and Inagaki, T.
SAE Technical Paper, 1991 , doi:10.4271/912069

911994

An Acrobatic Airship ‘ACROSTAT’

Onda, M. and Morikawa, Y.
SAE Technical Paper, 1991 , doi:10.4271/911994

912169

A Ground Test Program to Support Condition Monitoring of a Spacecraft Attitude Control Propulsion System

Clark, D., Lester, R., Baroth, E., and Coleman, A.
SAE Technical Paper, 1991 , doi:10.4271/912169

911105

Design and First Flight Results

Rovner, D.
SAE Technical Paper, 1991 , doi:10.4271/911105

910662

Improvement of Vehicle Motion and Riding-Comfort by Active Controlled Suspension System

Yasuda, E., Doi, S., Hattori, K., Suzuki, H. et al.
SAE Technical Paper, 1991 , doi:10.4271/910662

900567

Driver Attitudes and Behaviors

Flannagan, M. and Sivak, M.
SAE Technical Paper, 1990 , doi:10.4271/900567

861801

Airbus A320 Side Stick and Fly By Wire — An Update

Corps, S.
SAE Technical Paper, 1986 , doi:10.4271/861801

830759

A New Sensor Approach to an Attitude/Heading Reference System

Hemmel, D. and Rider, B.
SAE Technical Paper, 1983 , doi:10.4271/830759

820450

An Approach to the Application of Fuel Injection Equipment for Passenger Car Diesel Engines

Walz, L.
SAE Technical Paper, 1982 , doi:10.4271/820450

801177

Air Combat Advantages from Reaction Control Systems

Lacey, D.
SAE Technical Paper, 1980 , doi:10.4271/801177

801167

Strap down Navigation Comes of Age

BjornDahl, D.
SAE Technical Paper, 1980 , doi:10.4271/801167

750217

A Cybernetically Coupled Research Vehicle

Beck, R. and Kamm, I.
SAE Technical Paper, 1975 , doi:10.4271/750217

751046

Fly-By-Wire Flight Control System Design Considerations for Fighter Aircraft

Livingston, E.
SAE Technical Paper, 1975 , doi:10.4271/751046

740481

Integrated Flight/Propulsion Control Design Techniques Starting with the Engine

Sevich, G. and Beattie, E.
SAE Technical Paper, 1974 , doi:10.4271/740481

740351

Applications of Fluidics to Light Aircraft Instrumentation and Control

Garner, H.
SAE Technical Paper, 1974 , doi:10.4271/740351

740874

Three-Axis Attitude Control for Solar-Powered Electric Propulsion Spacecraft

Bouvier, H.
SAE Technical Paper, 1974 , doi:10.4271/740874

730304

Separate Surfaces for Automatic Flight Controls

Roskam, J., Barber, M., and Loschke, P.
SAE Technical Paper, 1973 , doi:10.4271/730304

730321

Application of Advanced Control System and Display Technology to General Aviation

Barber, M.
SAE Technical Paper, 1973 , doi:10.4271/730321

730317

NASA in General Aviation Research Past-Present-Future

Winblade, R.
SAE Technical Paper, 1973 , doi:10.4271/730317

730331

Development of a Low-Cost Flight Director System for General Aviation

Gee, S. and Servais, N.
SAE Technical Paper, 1973 , doi:10.4271/730331

730942

The Evaluation of Thrust Vector Control Systems for Advanced, Controllable, Solid-propelled Interceptor Motors

Sayles, D.
SAE Technical Paper, 1973 , doi:10.4271/730942

720316

Flight Evaluations of the Effect of Advanced Control Systems and Displays on the Handling Qualities of a General Aviation Airplane

Loschke, P., Barber, M., Jarvis, C., and Enevoldson, E.
SAE Technical Paper, 1972 , doi:10.4271/720316

720331

An Improved Stall Warning System for General Aviation Aircraft

Donnelly, T.
SAE Technical Paper, 1972 , doi:10.4271/720331

700803

Design and Fabrication of Small H2/O2 Engines

Domokos, S. and Falkenstein, G.
SAE Technical Paper, 1970 , doi:10.4271/700803

700783

A New Reaction Control Approach for Sounding Rockets

Honda, T., Keltz, W., Gabris, E., and Murphy, J.
SAE Technical Paper, 1970 , doi:10.4271/700783

700780

Compatibility of Warm Gas Reaction Controls with Solid Propellant Exhaust Product Used on Ballistic Missiles

Hyman, S.
SAE Technical Paper, 1970 , doi:10.4271/700780

700777

Lockseal for Thrust Vector Control of Rocket Motors

Moody, D.
SAE Technical Paper, 1970 , doi:10.4271/700777

700778

New Missile Control Applications for the Directed Jet Valve

McFall, R.
SAE Technical Paper, 1970 , doi:10.4271/700778

690326

Outside Looking In Attitude Gyros

Bonnell, C.
SAE Technical Paper, 1969 , doi:10.4271/690326

690693

VTOL Flight Investigation to Develop a Decelerating Instrument Approach Capability

Garren, J., Kelly, J., and Sommer, R.
SAE Technical Paper, 1969 , doi:10.4271/690693

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