Aircraft Engineering and Aerospace Technology: Volume 80 Issue 1
Strapline:
An International JournalTable of contents
Satellite attitude control by integrator back‐stepping with internal stabilization
Reşat Özgür Doruk, Erol KocaoğlanThis paper aims to focus on the implementation of the integral back‐stepping control on the model of BILSAT – 1 satellite of the Turkish Scientific and Technological Research…
Simplest AB‐thermonuclear space propulsion and electric generator
Alexander BolonkinThis paper aims to suggest a new thermonuclear space propulsion and electric generator for aerospace.
Design and optimization of interplanetary low‐thrust trajectory with planetary aerogravity‐assist maneuver
Haibin Shang, Pingyuan Cui, Enjie LuanThe purpose of this paper is to study the application of the planetary aerogravity‐assist (AGA) technique to the interplanetary transfer mission with low‐thrust engine, and the…
Control system design of multivariable non‐linear space robots
Amir NassirharandThe paper's purpose is to initiate an effort that will result in a systematic approach for design of control systems for multivariable, nonlinear, and unstable space robots.
Influence of flexible interface on the performance of whole spacecraft vibration isolation
Liang Lu, Wenhu HuangAs the installation of the vibration isolation device to the spacecraft for the whole spacecraft vibration isolation, the interface structure is typically modeled as a rigid…
Novel design of actuator fault reconstruction
Jia‐hui Luan, Ting‐di ZhaoThis paper aims to present a novel fault estimator design scheme, in order to improve the practicability of the fault estimation.
Design and development of thermal test model of a micro‐satellite for thermal balance test
Gilbert Justin Jose Nesamani, Sunil Chandrakant Joshi, Zhanli Jin, Poh Keong Chan, Soon Cheng LeeThis paper seeks to provide an insight into the design and development of the thermal test model (TTM) of X‐Sat, a 120 kg class micro‐satellite, being developed at the Centre…
Robust stabilization of input‐delayed systems with design example for rocket motor control
Elbrous M. JafarovThis paper aims to use a new design approach based on a Lagrange mean value theorem for the stabilization of multivariable input‐delayed system by linear controller.
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb