A robust and high precision optimal explicit guidance scheme for solid motor propelled launch vehicles with thrust and drag uncertainty. Issue 13 (2nd October 2016)
- Record Type:
- Journal Article
- Title:
- A robust and high precision optimal explicit guidance scheme for solid motor propelled launch vehicles with thrust and drag uncertainty. Issue 13 (2nd October 2016)
- Main Title:
- A robust and high precision optimal explicit guidance scheme for solid motor propelled launch vehicles with thrust and drag uncertainty
- Authors:
- Maity, Arnab
Padhi, Radhakant
Mallaram, Sanjeev
Rao, G. Mallikarjuna
Manickavasagam, M. - Abstract:
- ABSTRACT: A new nonlinear optimal and explicit guidance law is presented in this paper for launch vehicles propelled by solid motors. It can ensure very high terminal precision despite not having the exact knowledge of the thrust–time curve apriori. This was motivated from using it for a carrier launch vehicle in a hypersonic mission, which demands an extremely narrow terminal accuracy window for the launch vehicle for successful initiation of operation of the hypersonic vehicle. The proposed explicit guidance scheme, which computes the optimal guidance command online, ensures the required stringent final conditions with high precision at the injection point. A key feature of the proposed guidance law is an innovative extension of the recently developed model predictive static programming guidance with flexible final time . A penalty function approach is also followed to meet the input and output inequality constraints throughout the vehicle trajectory. In this paper, the guidance law has been successfully validated from nonlinear six degree-of-freedom simulation studies by designing an inner-loop autopilot as well, which enhances confidence of its usefulness significantly. In addition to excellent nominal results, the proposed guidance has been found to have good robustness for perturbed cases as well.
- Is Part Of:
- International journal of systems science. Volume 47:Issue 13(2016)
- Journal:
- International journal of systems science
- Issue:
- Volume 47:Issue 13(2016)
- Issue Display:
- Volume 47, Issue 13 (2016)
- Year:
- 2016
- Volume:
- 47
- Issue:
- 13
- Issue Sort Value:
- 2016-0047-0013-0000
- Page Start:
- 3078
- Page End:
- 3097
- Publication Date:
- 2016-10-02
- Subjects:
- launch vehicle guidance -- flexible final time optimal control -- model predictive static programming -- MPSP guidance -- hypersonic launch vehicle control -- autopilot design -- six-DOF simulation
System analysis -- Periodicals
003.3 - Journal URLs:
- http://www.tandf.co.uk/journals/titles/00207721.asp ↗
http://www.tandfonline.com/ ↗ - DOI:
- 10.1080/00207721.2015.1088100 ↗
- Languages:
- English
- ISSNs:
- 0020-7721
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 4542.693000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 1713.xml