|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/183 ; 244/184 ; 364/428|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 27 인용 특허 : 0|
When an aircraft is operating in an asymmetrical flight condition, such as during a landing decrab maneuver or during inflight engine out, the pilot is normally required to make precise compensatory roll control inputs to keep the aircraft moving along its original track angle. The pilot is relieved of this compensatory roll control task by providing a control system which automatically banks the aircraft to maintain the flight of the aircraft along the selected track angle while in the asymmetrical flight condition. Further adjustments in the bank angle...
An aircraft track angle hold control system comprising: a. roll control surfaces capable of generating a rolling moment on the aircraft in flight; b. yaw control means for permitting a pilot to command the aircraft to assume a nonzero sideslip condition through a rudder pedal input wherein the yaw control means includes a maneuver command control system which interprets the rudder pedal input as a sideslip angle command and which uses feedback control means to position a yaw control surface of the aircraft in such manner as to cause an actual sideslip an...