Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
21963 | 342 | 20.4 | 24% |
Classes in level above (level 2) |
ID, lev. above |
Publications | Label for level above |
---|---|---|
1273 | 8321 | JOURNAL OF THE AMERICAN HELICOPTER SOCIETY//JOURNAL OF AIRCRAFT//VERTICA |
Terms with highest relevance score |
Rank | Term | Type of term | Relevance score (tfidf) |
Class's shr. of term's tot. occurrences |
Shr. of publ. in class containing term |
Num. of publ. in class |
---|---|---|---|---|---|---|
1 | DYNAM SYST CONTROL BRANCH | Address | 6 | 50% | 2% | 8 |
2 | AIRCRAFT PARAMETER ESTIMATION | Author keyword | 2 | 67% | 1% | 2 |
3 | FLIGHT DYNAM BRANCH | Address | 2 | 67% | 1% | 2 |
4 | AEROSP SOFTWARE TECHNOL | Address | 2 | 50% | 1% | 3 |
5 | AVIAT MECH ENGN | Address | 2 | 20% | 2% | 7 |
6 | AIRCRAFT SYSTEM IDENTIFICATION | Author keyword | 1 | 100% | 1% | 2 |
7 | FLIGHT PATH RECONSTRUCTION | Author keyword | 1 | 50% | 1% | 2 |
8 | HIGH FEEDBACK GAIN AUGMENTATION | Author keyword | 1 | 100% | 1% | 2 |
9 | DYNAM CONTROL BRANCH | Address | 1 | 33% | 1% | 3 |
10 | AERODYNAMIC MODELING | Author keyword | 1 | 22% | 1% | 4 |
Web of Science journal categories |
Author Key Words |
Key Words Plus |
Rank | Web of Science journal category | Relevance score (tfidf) |
Class's shr. of term's tot. occurrences |
Shr. of publ. in class containing term |
Num. of publ. in class |
---|---|---|---|---|---|
1 | UNSTABLE AIRCRAFT | 2 | 67% | 1% | 2 |
2 | MEASUREMENT NOISE | 1 | 25% | 1% | 5 |
3 | TILT ROTOR AIRCRAFT | 1 | 50% | 1% | 2 |
4 | VEHICLE SYSTEM IDENTIFICATION | 1 | 100% | 1% | 2 |
5 | DERIVATIVE MODELS | 1 | 40% | 1% | 2 |
6 | AERODYNAMIC PARAMETERS | 1 | 50% | 0% | 1 |
7 | FLIGHT CONTROL LAW | 1 | 50% | 0% | 1 |
8 | ROTORCRAFT SYSTEM IDENTIFICATION | 0 | 33% | 0% | 1 |
9 | STATE SPACE REPRESENTATION | 0 | 33% | 0% | 1 |
10 | ABRUPT WING STALL | 0 | 25% | 0% | 1 |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
Application of system identification to aircraft at NASA Langley Research Center | 2005 | 18 | 15 | 93% |
Non-linear aircraft flight path reconstruction review and new advances | 1999 | 19 | 5 | 100% |
Address terms |
Rank | Address term | Relevance score (tfidf) |
Class's shr. of term's tot. occurrences |
Shr. of publ. in class containing term |
Num. of publ. in class |
---|---|---|---|---|---|
1 | DYNAM SYST CONTROL BRANCH | 6 | 50% | 2.3% | 8 |
2 | FLIGHT DYNAM BRANCH | 2 | 67% | 0.6% | 2 |
3 | AEROSP SOFTWARE TECHNOL | 2 | 50% | 0.9% | 3 |
4 | AVIAT MECH ENGN | 2 | 20% | 2.0% | 7 |
5 | DYNAM CONTROL BRANCH | 1 | 33% | 0.9% | 3 |
6 | FLIGHT MECH CONTROL | 1 | 15% | 1.8% | 6 |
7 | FLIGHT SYST BRANCH | 1 | 50% | 0.3% | 1 |
8 | SYST IDENTIFICAT | 1 | 50% | 0.3% | 1 |
9 | TRAINING HUMAN TORS COCKPIT OPERAT | 1 | 50% | 0.3% | 1 |
10 | WIND TUNNEL TEST | 1 | 50% | 0.3% | 1 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000195956 | WINDSHEAR PROBLEMS//ABORT LANDING//WIND IDENTIFICATION |
2 | 0.0000139137 | UNIT MATH INFORMAT//CIRCUIT THEORY MEASUREMENT SCI MAT SCI//FORWARD ACCUMULATION |
3 | 0.0000135350 | GEODETIC COORDINATES//ELLIPSOIDAL NORMAL//MULTI HOLE PRESSURE PROBE |
4 | 0.0000127840 | QUADROTOR//QUADROTOR HELICOPTER//HELICOPTER CONTROL |
5 | 0.0000122736 | FLIGHT TRAJECTORY DYNAM CONTROLS BRANCH//MOTION CUEING//BIODYNAMIC FEEDTHROUGH BDFT |
6 | 0.0000122106 | AV CONTROL//AVION CONTROL//ADAPTIVE WINGS |
7 | 0.0000120041 | INVERSE SIMULATION//FLIGHT DYNAMICS MODELING//PROPELLER DRIVEN AIRPLANE |
8 | 0.0000114760 | CONTROL ALLOCATION//CONTROL OF UAVS//DIRECT ALLOCATION |
9 | 0.0000106811 | FLEXIBLE AIR BREATHING HYPERSONIC VEHICLE//FLEXIBLE AIR BREATHING HYPERSONIC VEHICLE FAHV//AIRBREATHING HYPERSONIC VEHICLE |
10 | 0.0000095186 | JOURNAL OF THE AMERICAN HELICOPTER SOCIETY//VERTICA//ALFRED GESSOW ROTORCRAFT |