2020
DOI: 10.1108/aeat-12-2019-0241
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The airplane trim system – new functionalities

Abstract: Purpose A standard automatic flight control system – autopilot – will become required equipment of the future aircraft, operating in the common sky. For a specific group of aircraft, they are too expensive and too energy-consuming solutions. This paper aims to present the concept of an automatic flight control system that overcomes those limitations. Design/methodology/approach The proposed automatic flight control system uses the trim tabs in all prime flight controlling surfaces: elevator, ailerons and rud… Show more

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Cited by 6 publications
(5 citation statements)
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“…The set of tests preceded the installation of the stabilization system's hardware modules on the airplane, according to the DO-160G environmental standard requirements. After passing laboratory tests [12,13], the system was installed on PZL 130 TC-II Orlik The possibility of applying the developed system to stabilize the launch airplane flight was tested and confirmed within the flight velocities from the landing approach velocity up to the maximum operational velocity.…”
Section: Installation On Aircraft and Ground Testsmentioning
confidence: 99%
See 2 more Smart Citations
“…The set of tests preceded the installation of the stabilization system's hardware modules on the airplane, according to the DO-160G environmental standard requirements. After passing laboratory tests [12,13], the system was installed on PZL 130 TC-II Orlik The possibility of applying the developed system to stabilize the launch airplane flight was tested and confirmed within the flight velocities from the landing approach velocity up to the maximum operational velocity.…”
Section: Installation On Aircraft and Ground Testsmentioning
confidence: 99%
“…The set of tests preceded the installation of the stabilization system's hardware modules on the airplane, according to the DO-160G environmental standard requirements. After passing laboratory tests [12,13], the system was installed on PZL 130 TC-II Orlik…”
Section: Installation On Aircraft and Ground Testsmentioning
confidence: 99%
See 1 more Smart Citation
“…To stabilize and control the steady flights of an aircraft, Szczepanski proposed an automatic flight control system by the trim tabs in all prime flight controlling surfaces: the elevator, aileron, and rudder. 9 The stabilization of the flight was investigated in the performed test scenarios. A three-surface aircraft (TSA) configuration trim analysis is presented in the study by Goetzendorf-Grabowski et al 10 In his work, Goraj computed trim conditions using the STB software.…”
Section: Introductionmentioning
confidence: 99%
“…Nowadays, automatic flight control is regularly used in civil and military aircraft as well as for unmanned aerial vehicles (UAVs). Nevertheless, growing interest in what these systems are capable of offering makes it necessary to develop newer and more specialised functionalities (Szczepanski et al, 2020;Kuliberda, 2015;Jouhaud, 2013). Varieties of automatic systems have been used in aircraft for many years to stabilise flight parameters, such as spatial orientation, heading, altitude, speed, flight trajectory and others.…”
Section: Introductionmentioning
confidence: 99%