Active rotor control for helicopters: motivation and survey on higher harmonic control
Since the early helicopter developments, these aircraft have made a tremendous progress in performance, handling qualities, comfort and efficiency. However, modern helicopters still suffer from many problems that hinder a further increase in their efficiency, acceptance and hence their market share....
Saved in:
Published in: | CEAS aeronautical journal Vol. 1; no. 1-4; pp. 3 - 22 |
---|---|
Main Author: | |
Format: | Journal Article |
Language: | English |
Published: |
Vienna
Springer Vienna
2011
|
Subjects: | |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Abstract | Since the early helicopter developments, these aircraft have made a tremendous progress in performance, handling qualities, comfort and efficiency. However, modern helicopters still suffer from many problems that hinder a further increase in their efficiency, acceptance and hence their market share. The high level of vibrations and the noise generated by the rotor are the most important reasons for this. While vibrations are a concern of pilot and passenger comfort, they also give rise to an increase in maintenance efforts and costs. The high noise level limits the acceptance of helicopters in the public, e.g. landing of helicopters on or close to hospitals during EMS missions. High noise levels also lead to an early aural detection during military missions. Further drawbacks of helicopters are the high fuel consumption in high speed forward flight due to the excessive power required, the limited speed of flight, the low range for the same reason, low lead-lag damping, etc. To alleviate these drawbacks of helicopters, active rotor control technologies have been investigated for a long time. Many different approaches have been investigated and most of them are not being followed any more. First investigations started with so-called Higher Harmonic Control (HHC) which has been replaced by Individual Blade Control (IBC). The paper gives a survey of the typical problems and explains the vibration and noise issues in more detail. Since active means have to compete with passive ones, such methods are also briefly addressed. Next, the paper gives a review on important HHC achievements. Due to space constraints, the paper mainly focuses on wind tunnel and flight test results. A second paper reviews IBC and gives an outlook on the idea of the swashplateless helicopter. |
---|---|
AbstractList | Since the early helicopter developments, these aircraft have made a tremendous progress in performance, handling qualities, comfort and efficiency. However, modern helicopters still suffer from many problems that hinder a further increase in their efficiency, acceptance and hence their market share. The high level of vibrations and the noise generated by the rotor are the most important reasons for this. While vibrations are a concern of pilot and passenger comfort, they also give rise to an increase in maintenance efforts and costs. The high noise level limits the acceptance of helicopters in the public, e.g. landing of helicopters on or close to hospitals during EMS missions. High noise levels also lead to an early aural detection during military missions. Further drawbacks of helicopters are the high fuel consumption in high speed forward flight due to the excessive power required, the limited speed of flight, the low range for the same reason, low lead-lag damping, etc. To alleviate these drawbacks of helicopters, active rotor control technologies have been investigated for a long time. Many different approaches have been investigated and most of them are not being followed any more. First investigations started with so-called Higher Harmonic Control (HHC) which has been replaced by Individual Blade Control (IBC). The paper gives a survey of the typical problems and explains the vibration and noise issues in more detail. Since active means have to compete with passive ones, such methods are also briefly addressed. Next, the paper gives a review on important HHC achievements. Due to space constraints, the paper mainly focuses on wind tunnel and flight test results. A second paper reviews IBC and gives an outlook on the idea of the swashplateless helicopter. |
Author | Kessler, Ch |
Author_xml | – sequence: 1 givenname: Ch surname: Kessler fullname: Kessler, Ch email: christoph.kessler@dlr.de organization: DLR, Institute of Flight Systems |
BookMark | eNp9kE9PAjEQxRuDiYh8AG_9Aqsz_bNsvRGiYkLiRb02pe3CEmhJu5Dw7S1BPXqaN5P3Xia_WzIIMXhC7hEeEGDymJGzCasAsQIAWakrMsSmVpWUCgZ_umE3ZJzzpnigBi6kGJKvqe27o6cp9jFRG0Of4pa2Ra_9trNx3_uUn-guFpfpuxioCY7mQzr6Ey3bulutfTGbtIuhs78Nd-S6Ndvsxz9zRD5fnj9m82rx_vo2my4qy4CrigtobcOdQwsOpV26lkklnDCinCaNsrhkwqKsQTioDW-hUQ1KMJ4Lj46PCF56bYo5J9_qfep2Jp00gj6z0Rc2urDRZzZalQy7ZHLxhpVPehMPKZQ3_wl9A458aXw |
CitedBy_id | crossref_primary_10_1088_1742_6596_2367_1_012002 crossref_primary_10_1007_s13272_018_0323_2 crossref_primary_10_1155_2018_2870896 crossref_primary_10_1016_j_ifacol_2015_08_094 crossref_primary_10_1016_j_ymssp_2021_107739 crossref_primary_10_3390_aerospace10070623 crossref_primary_10_1016_j_ast_2019_105456 crossref_primary_10_1007_s13272_015_0157_0 crossref_primary_10_1007_s13272_024_00731_z crossref_primary_10_6112_kscfe_2013_18_3_060 crossref_primary_10_1017_aer_2021_94 crossref_primary_10_1016_j_ast_2018_03_026 crossref_primary_10_3182_20140824_6_ZA_1003_02740 crossref_primary_10_1016_j_ifacol_2015_11_122 crossref_primary_10_2514_1_G003512 crossref_primary_10_1016_j_cja_2015_08_010 crossref_primary_10_1177_10775463241259568 crossref_primary_10_1007_s13272_017_0265_0 crossref_primary_10_1016_j_jsv_2021_115980 crossref_primary_10_2514_1_J053195 crossref_primary_10_5050_KSNVE_2021_31_3_247 crossref_primary_10_1016_j_paerosci_2013_04_003 |
Cites_doi | 10.2514/3.57601 10.1016/j.ast.2004.01.001 10.1108/eb033000 10.1037/e429722004-001 10.21236/AD0766307 |
ContentType | Journal Article |
Copyright | Deutsches Zentrum für Luft- und Raumfahrt e.V. 2011 |
Copyright_xml | – notice: Deutsches Zentrum für Luft- und Raumfahrt e.V. 2011 |
DBID | AAYXX CITATION |
DOI | 10.1007/s13272-011-0005-9 |
DatabaseName | CrossRef |
DatabaseTitle | CrossRef |
DatabaseTitleList | |
DeliveryMethod | fulltext_linktorsrc |
Discipline | Engineering |
EISSN | 1869-5590 |
EndPage | 22 |
ExternalDocumentID | 10_1007_s13272_011_0005_9 |
GroupedDBID | -EM 06D 0R~ 0VY 1N0 203 29~ 2JY 2VQ 30V 4.4 406 408 409 40D 96X AAAVM AAFGU AAHNG AAIAL AAJKR AANZL AAPBV AARHV AARTL AATNV AATVU AAUYE AAWCG AAYFA AAYIU AAYQN AAYTO AAZMS ABBXA ABDZT ABECU ABFGW ABFTV ABHQN ABJNI ABJOX ABKAS ABKCH ABMQK ABQBU ABSXP ABTEG ABTHY ABTKH ABTMW ABULA ABWNU ABXPI ACBMV ACBRV ACBYP ACGFS ACHSB ACIGE ACIPQ ACKNC ACMLO ACOKC ACREN ACTTH ACVWB ACWMK ADHHG ADINQ ADKNI ADKPE ADMDM ADOXG ADRFC ADTPH ADURQ ADYFF ADYOE ADZKW AEBTG AEFTE AEGNC AEJHL AEJRE AEOHA AEPYU AESKC AESTI AETCA AEVLU AEVTX AEXYK AFLOW AFNRJ AFQWF AFWTZ AFYQB AFZKB AGAYW AGDGC AGGBP AGJBK AGMZJ AGQMX AGWZB AGYKE AHAVH AHBYD AHKAY AHSBF AHYZX AIAKS AIIXL AILAN AIMYW AITGF AJBLW AJDOV AJRNO AJZVZ AKLTO AKQUC ALFXC ALMA_UNASSIGNED_HOLDINGS AMKLP AMTXH AMXSW AMYLF AMYQR ANMIH AUKKA AXYYD AYJHY BGNMA CSCUP DNIVK DPUIP EBLON EBS EIOEI EJD FERAY FIGPU FINBP FNLPD FRRFC FSGXE FYJPI GGCAI GGRSB GJIRD GQ6 GQ7 GQ8 HF~ HMJXF HQYDN HRMNR HZ~ I0C IKXTQ IWAJR IXD IZIGR J-C J0Z JBSCW JCJTX JZLTJ KOV LLZTM M4Y NPVJJ NQJWS NU0 O9- O93 O9I O9J P9P PT4 QOS R89 R9I RLLFE ROL RSV S1Z S27 S3B SEG SHX SISQX SNE SNPRN SNX SOHCF SOJ SPISZ SRMVM SSLCW STPWE T13 TSG U2A UG4 UOJIU UTJUX UZXMN VFIZW W48 WK8 Z45 Z7R Z7S Z7X ZMTXR ~A9 AACDK AAJBT AASML AAYXX ABAKF ACAOD ACDTI ACZOJ AEFQL AEMSY AFBBN AGQEE AGRTI AIGIU CITATION H13 SJYHP |
ID | FETCH-LOGICAL-c2039-340fc83dd1c0d15cbdf2594d4a4d1c789c1b24c15604d06a3f0898150ae34e1d3 |
IEDL.DBID | AEJHL |
ISSN | 1869-5582 |
IngestDate | Thu Sep 12 16:55:36 EDT 2024 Sat Dec 16 12:04:33 EST 2023 |
IsPeerReviewed | false |
IsScholarly | true |
Issue | 1-4 |
Keywords | Helicopter noise Active rotor control Higher Harmonic Control Individual Blade Control Helicopter vibrations |
Language | English |
LinkModel | DirectLink |
MergedId | FETCHMERGED-LOGICAL-c2039-340fc83dd1c0d15cbdf2594d4a4d1c789c1b24c15604d06a3f0898150ae34e1d3 |
PageCount | 20 |
ParticipantIDs | crossref_primary_10_1007_s13272_011_0005_9 springer_journals_10_1007_s13272_011_0005_9 |
PublicationCentury | 2000 |
PublicationDate | 9-2011 |
PublicationDateYYYYMMDD | 2011-01-01 |
PublicationDate_xml | – year: 2011 text: 9-2011 |
PublicationDecade | 2010 |
PublicationPlace | Vienna |
PublicationPlace_xml | – name: Vienna |
PublicationSubtitle | An Official Journal of the Council of European Aerospace Societies |
PublicationTitle | CEAS aeronautical journal |
PublicationTitleAbbrev | CEAS Aeronaut J |
PublicationYear | 2011 |
Publisher | Springer Vienna |
Publisher_xml | – name: Springer Vienna |
References | Yen (CR25) 1981; 18 Kube (CR31) 1992; 37 Shaw, Albion (CR26) 1981; 26 CR19 CR18 Braun (CR3) 1982; 27 Leishman (CR12) 2006 CR15 O’Leary, Miao (CR28) 1982; 27 CR14 CR13 CR35 Shaw, Albion, Hanker, Teal (CR27) 1989; 34 CR34 Reichert (CR1) 1981; 5 CR11 CR10 CR32 Achache, Polychroniadis (CR33) 1987; 11 Brooks, Booth (CR38) 1993; 38 Loewy (CR2) 1984; 29 Hammond (CR22) 1983; 28 du Val, Gregory, Gupta (CR29) 1984; 29 Lehmann (CR30) 1985; 9 CR4 CR6 CR5 CR8 CR7 CR9 Arcidiacono (CR17) 1961; 6 Nygen, Schrage (CR36) 1989; 34 Payne (CR16) 1958; 30 CR23 Wood, Powers, Cline, Hammond (CR24) 1985; 30 CR21 CR43 CR20 CR42 CR41 Splettstoesser, Schultz, Kube, Brooks, Booth, Niesl, Streby (CR39) 1994; 39 CR40 Nguyen, Chopra (CR37) 1990; 35 van der Wall, Burley, Yu, Richard, Pengel, Beaumier (CR44) 2004; 8 K Nguyen (5_CR37) 1990; 35 5_CR8 J Shaw (5_CR27) 1989; 34 5_CR7 WR Splettstoesser (5_CR39) 1994; 39 5_CR6 5_CR5 ER Wood (5_CR24) 1985; 30 5_CR4 PR Payne (5_CR16) 1958; 30 5_CR13 RW Val du (5_CR29) 1984; 29 5_CR35 5_CR34 5_CR11 5_CR10 5_CR32 5_CR15 D Braun (5_CR3) 1982; 27 5_CR14 J Shaw (5_CR26) 1981; 26 CE Hammond (5_CR22) 1983; 28 JG Leishman (5_CR12) 2006 BG Wall van der (5_CR44) 2004; 8 5_CR19 RG Loewy (5_CR2) 1984; 29 5_CR18 R Kube (5_CR31) 1992; 37 JG Yen (5_CR25) 1981; 18 M Achache (5_CR33) 1987; 11 G Reichert (5_CR1) 1981; 5 5_CR23 PJ Arcidiacono (5_CR17) 1961; 6 J O’Leary (5_CR28) 1982; 27 5_CR21 5_CR43 TF Brooks (5_CR38) 1993; 38 5_CR9 G Lehmann (5_CR30) 1985; 9 5_CR20 5_CR42 KP Nygen (5_CR36) 1989; 34 5_CR41 5_CR40 |
References_xml | – ident: CR18 – ident: CR43 – volume: 9 start-page: 273 issue: 3 year: 1985 end-page: 284 ident: CR30 article-title: The effect of higher harmonic control (HHC) on a four-bladed hingeless model rotor publication-title: Vertica contributor: fullname: Lehmann – ident: CR4 – ident: CR14 – volume: 26 start-page: 32 issue: 3 year: 1981 end-page: 39 ident: CR26 article-title: Active control of the helicopter rotor for vibration reduction publication-title: J AHS contributor: fullname: Albion – volume: 29 start-page: 4 issue: 4 year: 1984 end-page: 30 ident: CR2 article-title: Helicopter vibrations: a technological perspective publication-title: J AHS contributor: fullname: Loewy – volume: 27 start-page: 52 issue: 1 year: 1982 end-page: 57 ident: CR28 article-title: Design of higher harmonic control for the ABC publication-title: J AHS contributor: fullname: Miao – volume: 30 start-page: 3 issue: 1 year: 1985 end-page: 20 ident: CR24 article-title: On developing and flight testing a higher harmonic control system publication-title: J AHS contributor: fullname: Hammond – ident: CR10 – volume: 18 start-page: 1064 issue: 12 year: 1981 end-page: 1069 ident: CR25 article-title: Higher harmonic control for helicopters with two-bladed and four-bladed rotors publication-title: J Aircr doi: 10.2514/3.57601 contributor: fullname: Yen – volume: 38 start-page: 45 issue: 3 year: 1993 end-page: 55 ident: CR38 article-title: The effects of higher harmonic control on blade-vortex interaction noise and vibration publication-title: J AHS contributor: fullname: Booth – ident: CR35 – ident: CR6 – ident: CR8 – volume: 27 start-page: 37 issue: 4 year: 1982 ident: CR3 article-title: Development of antiresonance force isolators for helicopter vibration reduction publication-title: J AHS contributor: fullname: Braun – ident: CR40 – ident: CR42 – ident: CR23 – volume: 29 start-page: 30 issue: 3 year: 1984 end-page: 37 ident: CR29 article-title: Design and evaluation of a state-feedback vibration controller publication-title: J AHS contributor: fullname: Gupta – volume: 6 start-page: 8 issue: 8 year: 1961 end-page: 19 ident: CR17 article-title: Theoretical performance of helicopters having second and higher harmonic feathering control publication-title: J AHS contributor: fullname: Arcidiacono – ident: CR21 – ident: CR19 – volume: 34 start-page: 51 issue: 3 year: 1989 end-page: 58 ident: CR36 article-title: Fixed-gain versus adaptive higher harmonic control simulation publication-title: J AHS contributor: fullname: Schrage – ident: CR15 – volume: 34 start-page: 14 issue: 1 year: 1989 end-page: 25 ident: CR27 article-title: Higher harmonic control: wind tunnel demonstration of fully effective vibration hub force suppression publication-title: J AHS contributor: fullname: Teal – ident: CR13 – volume: 37 start-page: 61 issue: 3 year: 1992 end-page: 68 ident: CR31 article-title: New aspects of higher harmonic control on a four-bladed hingeless model rotor publication-title: J AHS contributor: fullname: Kube – volume: 8 start-page: 273 issue: 4 year: 2004 end-page: 284 ident: CR44 article-title: The HART II test-measurement of helicopter rotor wakes publication-title: Aerosp Sci Technol doi: 10.1016/j.ast.2004.01.001 contributor: fullname: Beaumier – ident: CR11 – ident: CR9 – volume: 30 start-page: 222 issue: 8 year: 1958 end-page: 226 ident: CR16 article-title: Higher harmonic rotor control: the possibilities of third and higher harmonic feathering for delaying the stall limit in helicopters publication-title: Aircr Eng doi: 10.1108/eb033000 contributor: fullname: Payne – volume: 39 start-page: 3 issue: 4 year: 1994 end-page: 13 ident: CR39 article-title: A higher harmonic control test in the DNW to reduce impulsive BVI noise publication-title: J AHS contributor: fullname: Streby – ident: CR32 – volume: 11 start-page: 123 issue: 1/2 year: 1987 end-page: 138 ident: CR33 article-title: Development of an experimental systems for active control of vibrations on helicopters—development methodology for an Airborne System publication-title: Vertica contributor: fullname: Polychroniadis – ident: CR34 – ident: CR5 – ident: CR7 – year: 2006 ident: CR12 publication-title: Principles of Helicopter Aerodynamics contributor: fullname: Leishman – volume: 28 start-page: 10 issue: 1 year: 1983 end-page: 15 ident: CR22 article-title: Wind tunnel results showing rotor vibratory loads reduction using higher harmonic blade pitch publication-title: J AHS contributor: fullname: Hammond – volume: 35 start-page: 78 issue: 3 year: 1990 end-page: 89 ident: CR37 article-title: Application of higher harmonic control to rotors operating at high speed and thrust publication-title: J AHS contributor: fullname: Chopra – ident: CR41 – volume: 5 start-page: 1 issue: 1 year: 1981 end-page: 20 ident: CR1 article-title: Helicopter vibration control—a survey publication-title: Vertica contributor: fullname: Reichert – ident: CR20 – ident: 5_CR42 – volume-title: Principles of Helicopter Aerodynamics year: 2006 ident: 5_CR12 contributor: fullname: JG Leishman – ident: 5_CR19 – ident: 5_CR23 – volume: 35 start-page: 78 issue: 3 year: 1990 ident: 5_CR37 publication-title: J AHS contributor: fullname: K Nguyen – ident: 5_CR21 – volume: 5 start-page: 1 issue: 1 year: 1981 ident: 5_CR1 publication-title: Vertica contributor: fullname: G Reichert – ident: 5_CR40 – volume: 30 start-page: 3 issue: 1 year: 1985 ident: 5_CR24 publication-title: J AHS contributor: fullname: ER Wood – volume: 38 start-page: 45 issue: 3 year: 1993 ident: 5_CR38 publication-title: J AHS contributor: fullname: TF Brooks – volume: 30 start-page: 222 issue: 8 year: 1958 ident: 5_CR16 publication-title: Aircr Eng doi: 10.1108/eb033000 contributor: fullname: PR Payne – volume: 34 start-page: 51 issue: 3 year: 1989 ident: 5_CR36 publication-title: J AHS contributor: fullname: KP Nygen – ident: 5_CR5 – ident: 5_CR6 doi: 10.1037/e429722004-001 – volume: 8 start-page: 273 issue: 4 year: 2004 ident: 5_CR44 publication-title: Aerosp Sci Technol doi: 10.1016/j.ast.2004.01.001 contributor: fullname: BG Wall van der – ident: 5_CR8 doi: 10.21236/AD0766307 – ident: 5_CR9 – ident: 5_CR34 – ident: 5_CR7 – volume: 28 start-page: 10 issue: 1 year: 1983 ident: 5_CR22 publication-title: J AHS contributor: fullname: CE Hammond – ident: 5_CR15 – volume: 9 start-page: 273 issue: 3 year: 1985 ident: 5_CR30 publication-title: Vertica contributor: fullname: G Lehmann – ident: 5_CR32 – ident: 5_CR13 – ident: 5_CR11 – volume: 37 start-page: 61 issue: 3 year: 1992 ident: 5_CR31 publication-title: J AHS contributor: fullname: R Kube – ident: 5_CR41 – volume: 27 start-page: 52 issue: 1 year: 1982 ident: 5_CR28 publication-title: J AHS contributor: fullname: J O’Leary – volume: 27 start-page: 37 issue: 4 year: 1982 ident: 5_CR3 publication-title: J AHS contributor: fullname: D Braun – volume: 6 start-page: 8 issue: 8 year: 1961 ident: 5_CR17 publication-title: J AHS contributor: fullname: PJ Arcidiacono – ident: 5_CR18 – ident: 5_CR43 – volume: 29 start-page: 30 issue: 3 year: 1984 ident: 5_CR29 publication-title: J AHS contributor: fullname: RW Val du – volume: 39 start-page: 3 issue: 4 year: 1994 ident: 5_CR39 publication-title: J AHS contributor: fullname: WR Splettstoesser – volume: 29 start-page: 4 issue: 4 year: 1984 ident: 5_CR2 publication-title: J AHS contributor: fullname: RG Loewy – ident: 5_CR20 – ident: 5_CR4 – volume: 34 start-page: 14 issue: 1 year: 1989 ident: 5_CR27 publication-title: J AHS contributor: fullname: J Shaw – volume: 26 start-page: 32 issue: 3 year: 1981 ident: 5_CR26 publication-title: J AHS contributor: fullname: J Shaw – volume: 18 start-page: 1064 issue: 12 year: 1981 ident: 5_CR25 publication-title: J Aircr doi: 10.2514/3.57601 contributor: fullname: JG Yen – volume: 11 start-page: 123 issue: 1/2 year: 1987 ident: 5_CR33 publication-title: Vertica contributor: fullname: M Achache – ident: 5_CR35 – ident: 5_CR14 – ident: 5_CR10 |
SSID | ssj0000603454 |
Score | 2.0393217 |
Snippet | Since the early helicopter developments, these aircraft have made a tremendous progress in performance, handling qualities, comfort and efficiency. However,... |
SourceID | crossref springer |
SourceType | Aggregation Database Publisher |
StartPage | 3 |
SubjectTerms | Aerospace Technology and Astronautics Engineering Review Paper |
Title | Active rotor control for helicopters: motivation and survey on higher harmonic control |
URI | https://link.springer.com/article/10.1007/s13272-011-0005-9 |
Volume | 1 |
hasFullText | 1 |
inHoldings | 1 |
isFullTextHit | |
isPrint | |
link | http://sdu.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwnV1LSwMxEB5se9GDb7G-yMGTEkk2SZt4K9pSRLz4wNuS11JQt6W1gv_eZLvbWtCDwl52CcMyTDKT-Wa-ATglmZJWZQY7pjTmynhsvGthF5yfsZ4YaovUxX377lledyNNTjJPXeQvFxUiWRzUi143lrRjFQGNjdACqxo0gusRog6NTvemfzvPrJAWYbwYfxbHLWEhZFLBmT_JWXZIy2ho4WR6G__5vU1YL0NK1JnZwBas-Hwb1r4RDe7AU6c41tB4GK7YqCxPRyFeRQP_GmxhFDk2L9HbfNgZ0rlDk-n4w3-i8DYoqkFQpLmOVLqVhF147HUfrvq4nKiAbRIhX8ZJZiVzjlriqLDGZeH6wx3XPHxqS2WpSbiN3dXckZZmGZFKhphRe8Y9dWwP6vkw9_uAuLYhsgjSDA0CEmOI1iQjOvg6Yph2TTir1JqOZsQZ6YIiOSorDcqK2LdIVRPOK62m5R6a_L764E-rD2F1lgeOzxHU38dTfwy1iZuelJbzBRKgvgg |
link.rule.ids | 315,782,786,27935,27936,41075,42144,48346,48349,48359,49651,49654,49664,52155 |
linkProvider | Springer Nature |
linkToHtml | http://sdu.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwnV1LTwIxEJ4oHNSDbyM-e_CkadLddmHrjQgEI3IRDZw2fW046EJATPz3tmUXJNGDJnvZTTPZTKad6Xwz3wBckZTHiqcSa8oFZlwaLI2uYm2dn1SGyED51MVTrduPG01Hk0OLXhhf7V5Akv6kXja70bDmyggC1wkdYb4OZUd2zkpQrvcHg8YitUKqhDI__8zNW8JRFIcFnvmTnFWPtAqHei_T2vnX_-3Cdh5UovrcCvZgzWT7sPWNavAAXur-YEOTkb1ko7xAHdmIFQ3Nq7WGsWPZvEVvi3FnSGQaTWeTD_OJ7NvQ14MgR3TtyHQLCYfw3Gr27to4n6mAVehAX8pIqmKqdaCIDiIldWovQEwzweynWsxVIEOmXH8106QqaEpiHtuoURjKTKDpEZSyUWaOATGhbGxhpcnACgilJEKQlAjr7YikQlfgutBrMp5TZyRLkmSnrMQqy6HfUcIrcFNoNcl30fT31Sd_Wn0JG-3eYyfp3HcfTmFznhV2zxmU3iczcw7rUz27yM3oC9lNwjo |
linkToPdf | http://sdu.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwpV1LSwMxEB5sC6IH32J95uBJCc1usu3GixTbalGKYBVvS15LD7otfQj-e5N9tBb0IMJesoQhDLM7k5n5vgE4JzEPFY8l1pQLzLg0WBpdx9o6P6kMkZ5KUxdPjd5r2Go7mpzrAguTdrsXJckM0-BYmpJpbaTj2gL4Rv2GaynwHCo6wLwEFZcVsyZeaXb7t515moXUCWXpLDQ3ewkHQegXtc2f5Cx7p-XSaOpxOpv_PusWbOTBJmpm1rENKybZgfVvFIS78NJMf3hoPLSXb5Q3riMbyaKBebNWMnLsm1fofT4GDYlEo8ls_GE-kV0N0j4R5AiwHcluIWEPnjvt_s0dzmctYOW7YjBlJFYh1dpTRHuBkjq2FyOmmWD2VSPkypM-Uw53zTSpCxqTkIc2mhSGMuNpug_lZJiYA0BMKBtzWGnSswJ8KYkQJCbCekEiqdBVuCh0HI0ySo1oQZ7slBVZZbmqeBDxKlwWGo7yr2vy--7DP-0-g9XHVid66Pbuj2AtSxa75xjK0_HMnEBpomenuUV9AaeEytE |
openUrl | ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.atitle=Active+rotor+control+for+helicopters%3A+motivation+and+survey+on+higher+harmonic+control&rft.jtitle=CEAS+aeronautical+journal&rft.au=Kessler%2C+Ch&rft.date=2011-01-01&rft.pub=Springer+Vienna&rft.issn=1869-5582&rft.eissn=1869-5590&rft.volume=1&rft.issue=1-4&rft_id=info:doi/10.1007%2Fs13272-011-0005-9&rft.externalDocID=10_1007_s13272_011_0005_9 |
thumbnail_l | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1869-5582&client=summon |
thumbnail_m | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1869-5582&client=summon |
thumbnail_s | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1869-5582&client=summon |