JPH0411440B2 - - Google Patents
Info
- Publication number
- JPH0411440B2 JPH0411440B2 JP17109985A JP17109985A JPH0411440B2 JP H0411440 B2 JPH0411440 B2 JP H0411440B2 JP 17109985 A JP17109985 A JP 17109985A JP 17109985 A JP17109985 A JP 17109985A JP H0411440 B2 JPH0411440 B2 JP H0411440B2
- Authority
- JP
- Japan
- Prior art keywords
- gust
- aircraft
- loop control
- control
- steering
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 238000000034 method Methods 0.000 claims description 14
- 238000001514 detection method Methods 0.000 claims description 12
- 230000000694 effects Effects 0.000 description 9
- 238000011045 prefiltration Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 6
- 238000004088 simulation Methods 0.000 description 3
- 230000001447 compensatory effect Effects 0.000 description 2
- 230000010355 oscillation Effects 0.000 description 2
- 238000001228 spectrum Methods 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000000452 restraining effect Effects 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
Landscapes
- Feedback Control In General (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Traffic Control Systems (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP17109985A JPS6231600A (ja) | 1985-08-05 | 1985-08-05 | 航空機の突風荷重軽減制御方式 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP17109985A JPS6231600A (ja) | 1985-08-05 | 1985-08-05 | 航空機の突風荷重軽減制御方式 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6231600A JPS6231600A (ja) | 1987-02-10 |
| JPH0411440B2 true JPH0411440B2 (de) | 1992-02-28 |
Family
ID=15916964
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP17109985A Granted JPS6231600A (ja) | 1985-08-05 | 1985-08-05 | 航空機の突風荷重軽減制御方式 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6231600A (de) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2566235B2 (ja) * | 1987-03-24 | 1996-12-25 | 防衛庁技術研究本部長 | 飛行制御装置 |
| FR2891802B1 (fr) * | 2005-10-11 | 2009-03-13 | Airbus France Sas | Procede et dispositif pour attenuer sur un aeronef les effets d'une turbulence verticale |
| EP1814006B1 (de) * | 2006-01-25 | 2016-09-21 | Airbus Opérations SAS | Minimierung der dynamischen strukturellen Lasten eines Flugzeuges |
| US9639089B2 (en) * | 2015-06-04 | 2017-05-02 | The Boeing Company | Gust compensation system and method for aircraft |
| JP6492138B2 (ja) | 2017-08-29 | 2019-03-27 | 株式会社Ｓｕｂａｒｕ | 航空機の翼荷重軽減装置及び航空機の翼荷重軽減方法 |
-
1985
- 1985-08-05 JP JP17109985A patent/JPS6231600A/ja active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6231600A (ja) | 1987-02-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6751529B1 (en) | System and method for controlling model aircraft | |
| US20140288731A1 (en) | Flight Control System | |
| US8818573B2 (en) | Method and device for detecting an uncontrolled movement of an aircraft control surface | |
| US20100145555A1 (en) | Flight Control System | |
| US3279725A (en) | Flight controller for flexible vehicles | |
| JPH0375399B2 (de) | ||
| Horn et al. | Use of rotor state feedback to improve closed-loop stability and handling qualities | |
| CN110647160A (zh) | 一种用于航空器的飞行控制方法和装置 | |
| US8620492B2 (en) | Yaw damping system and method for aircraft | |
| US7255306B2 (en) | Method and computer program product for controlling the control effectors of an aerodynamic vehicle | |
| Ahmad et al. | Dynamic modelling and linear quadratic Gaussian control of a twin-rotor multi-input multi-output system | |
| CN110825115A (zh) | 一种飞机迎角和过载的极限限制控制方法 | |
| Jacobson et al. | Residual pitch oscillation (RPO) flight test and analysis on the B-2 bomber | |
| Smerlas et al. | Evaluating H∞ controllers on the NRC Bell 205 fly-by-wire helicopter | |
| JPH0411440B2 (de) | ||
| CN111099012B (zh) | 用于缓解飞机的结构柔性模式激发的影响的系统和方法 | |
| Heinze et al. | Analysis and wind tunnel testing of a piezoelectric tab for aeroelastic control applications | |
| Andrighettoni et al. | Multi-input/multi-output adaptive active flutter suppression for a wing model | |
| Idan et al. | Off-line comparison of classical and robust flight simulator motion control | |
| US7548800B2 (en) | Method and computer program product for controlling an aerodynamic vehicle having at least one structural mode | |
| US20040104302A1 (en) | Method and system for reducing engine induced vibration amplitudes in an aircraft fuselage | |
| EP2146263B1 (de) | Mehrachsiges Modenunterdrückungssystem für Luftfahrzeug | |
| Hess | A model-based investigation of manipulator characteristics and pilot/vehicle performance | |
| Van der Weerd | Pilot-Induced Oscillation Suppression Methods and their Effects on Large Transport Aircraft Handling Qualities | |
| Ghiringhelli et al. | Multi-body analysis of an active control for a tiltrotor |