Applications of global positioning system velocity-based attitude information

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 5, 2001, Pages 998-1008

  Kornfeld, R P ^a   Hansman, R J ^a   Deyst, J J ^a   Amonlirdviman, K ^a   Walker, E M ^a  

^a MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CONTROL SYSTEM SYNTHESIS; ELECTRONIC GUIDANCE SYSTEMS; FLIGHT DYNAMICS; GLOBAL POSITIONING SYSTEM; TRAJECTORIES; VECTOR QUANTIZATION;

AIRCRAFT ATTITUDE INFORMATION; AIRCRAFT FLIGHT CONTROL LOOP; TUNNEL IN THE SKY TRAJECTORY GUIDANCE SYSTEMS; VELOCITY VECTOR MEASUREMENT;

VELOCITY CONTROL;

EID: 0035440801     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4808     Document Type: Article

References (8)

1. Attitude determination
2. Inertially aided GPS based attitude heading reference system (AHRS) for general aviation aircraft
3. Single-antenna GPS-based aircraft attitude determination
4. The impact of GPS velocity based flight control on flight instrumentation architecture
5. The use of pilot rating in the evaluation of aircraft handling qualities
6. GPS 3-D cockpit displays: Sensors, algorithms, and flight testing
7. Integrated design of a man-machine interface for 4-D navigation
8. Application of the analytic hierarchy process for making subjective comparisons between multiple automation/display options